Authors are listed alphabetically. To facilitate searching, use the index below. NOTE: only first author names are indexed.
A B C D E F G H I J K L M N O P Q R S T U V W X Y Z
ABBOTT, IRA H.; VON DOENHOFF, ALBERT E.; STIVERS, LOUIS S. ,. JR. Summary of airfoil data. NACA-TR-824 ; NACA-ACR-L5C05 ; NACA-WR-L-560
ALLEN, H. JULIAN Calculation of the chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing-edge flaps. NACA-TR-634
ALLEN, H. JULIAN A simplified method for the calculation of airfoil pressure distribution. NACA-TN-708
AMES, MILTON B. Wind-tunnel investigation of control-surface characteristics. III - A small aerodynamic balance of various nose shapes used with a 30-percent-chord flap on an NACA 0009 airfoil. NACA-WR-L-301 ; NACA-ARR-12
AMES, MILTON B.; EASTMAN, DONALD R. ,. JR. Wind-tunnel investigation of control-surface characteristics. IV - A medium aerodynamic balance of various nose shapes used with a 30-percent-chord flap on an NACA 0009 airfoil. NACA-WR-L-355 ; NACA-ARR-16
AMES, MILTON B.; SEARS, RICHARD I. Determination of control-surface characteristics from NACA plain-flap and tab data. NACA-TR-721 ; NACA-TN-796
AMES, MILTON B. ,. JR.; SEARS, RICHARD I. Pressure-distribution investigation on an NACA 0009 airfoil with a 30-percent-chord plain flap and three tabs. NACA-TN-759
AMES RESEARCH STAFF Equations, tables, and charts for compressible flow. NACA-TR-1135 ; NACA-TN-1428
ANDERSON, RAYMOND F. Determination of the characteristics of tapered wings. NACA-TR-572
BADER, W. Measurements on a low-wing model in the rotating jet and comparison with flight measurements. NACA-TM-910
BATES, WILLIAM R. Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates. NACA-TN-1291
BENNETT, CHARLES V.; JOHNSON, JOSEPH L. Experimental determination of the damping in roll and aileron rolling effectiveness of three wings having 2 degrees, 42 degrees, and 62 degrees sweepback. NACA-TN-1278 ; NACA-MR-L6F05
BIELAT, RALPH P. A simple method for estimating terminal velocity including effect of compressibility on drag. NACA-WR-L-78 ; NACA-ACR-L5G31
BIERMANN, DAVID; HARTMAN, EDWIN P. The aerodynamic characteristics of six full-scale propellers having different airfoil sections. NACA-TR-650
BIERMANN, DAVID; HARTMAN EDWIN P. Tests of two full-scale propellers with different pitch distributions, at blade angles up to 60 degrees. NACA-TR-658
BIRD, J. D. Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil. NACA-WR-L-172 ; NACA-ACR-L5F13A
BOWMAN, JAMES S. ,. JR. Summary of spin technology as related to light general-aviation airplanes. NASA-TN-D-6575
BURK, SANGER M. ,. JR. Summary of design considerations for airplane spin-recovery parachute systems. NASA-TN-D-6866
CAHILL, JONES F. Summary of section data on trailing-edge high-lift devices. NACA-TR-938 ; NACA-RM-L8D09
CAMPBELL, JOHN P.; MCKINNEY, MARION O. ,. JR. A study of the problem of designing airplanes with satisfactory inherent damping of the dutch roll oscillation. NACA-TR-1199 ; NACA-TN-3035
CAMPBELL, JOHN P.; MCKINNEY, MARION O. Summary of methods for calculating dynamic lateral stability and response and for estimating aerodynamic stability derivatives. NACA-TR-1098 ; NACA-TN-2409
CHAMBERS, J. R.; YIP, L. P.; MOUL, T. M. Wind-tunnel investigation of an advanced general aviation canard configuration. NASA-TM-85760
COE, PAUL L. ,. JR. Review of drag cleanup tests in Langley full-scale tunnel (from 1935 to 1945) applicable to current general aviation airplane. NASA-TN-D-8206
COHEN, DORIS A theoretical investigation of the rolling oscillations of an airplane with ailerons free. NACA-TR-787 ; NACA-TR-709 ; NACA-ARR-4A06 ; NACA-WR-L-361
COOPER, GEORGE E.; HARPER, ROBERT P. ,. JR. The use of pilot rating in the evaluation of aircraft handling qualities. NASA-TN-D-5153
CORRINGTON, LESTER C.; FISHER, WILLIAM F. Effect of preignition on cylinder temperatures, pressures, power output, and piston failures. NACA-TN-1637 ; NACA-RM-E6L10
CRANDALL, STEWART M.; MURRAY, HARRY E. Analysis of available data on the effects of tabs on control-surface hinge moments. NACA-TN-1049 ; NACA-MR-L5F12
CRANE, ROBERT M. Computation of hinge-moment characteristics of horizontal tails from section data. NACA-WR-A-11 ; NACA-CB-5B05
DEARBORN, C. H.; SILVERSTEIN, ABE Drag analysis of single-engine military airplanes tested in the NACA full-scale wind tunnel. NACA-WR-L-489
DEMING, A. F. Noise from propellers with symmetrical sections at zero blade angle. NACA-TN-605
DEYOUNG, JOHN Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds. NACA-TR-1071 ; NACA-TN-2278
DEYOUNG, JOHN; BARLING, WALTER H. ,. JR. Correction of additional span loadings computed by the Weissinger seven-point method for moderately tapered wings of high aspect ratio. NACA-TN-3500
DEYOUNG, JOHN; HARPER, CHARLES W. Theoretical symmetric span loading at subsonic speeds for wings having arbitrary plan form. NACA-TR-921 ; NACA-TN-1476 ; NACA-TN-1491 ; NACA-TN-1772
DIEHL, WALTER S. The mean aerodynamic chord and the aerodynamic center of a tapered wing. NACA-TR-751
DINGELDEIN, RICHARD C. Full-scale tunnel investigation of the pressure distribution over the tail of the P-47B airplane. NACA-WR-L-439 ; NACA-ARR-3E25
DODS, JULES B. ,. JR.; TINLING, BRUCE E. Summary of results of a wind-tunnel investigation of nine related horizontal tails. NACA-TN-3497 ; NACA-RM-A51G31A
DONEGAN, JAMES J. Matrix methods for determining the longitudinal-stability derivatives of an airplane from transient flight data. NACA-TR-1169 ; NACA-TN-2902
DONEGAN, JAMES J.; ROBINSON, SAMUEL W. ,. JR.; GATES, ORDWAY B. ,. JR. Determination of lateral-stability derivatives and transfer-function coefficients from frequency-response data for lateral motions. NACA-TR-1225 ; NACA-TN-3083
EGGLESTON, JOHN M.; MATHEWS, CHARLES W. Application of several methods for determining transfer functions and frequency response of aircraft from flight data. NACA-TR-1204 ; NACA-TN-2997
FINK, MARVIN P.; FREEMAN, DELMA C. ,. JR. Full-scale wind-tunnel investigation of static longitudinal and lateral characteristics of a light twin-engine airplane. NASA-TN-D-4983
FISCHEL, JACK Hinge moments of sealed-internal-balance arrangements for control surfaces II : experimental investigation of fabric seals in the presence of a thin-plate overhang. NACA-WR-L-52 ; NACA-L5F30A
FISCHEL, JACK; IVEY, MARGARET F. Collection of the test data for lateral control with full-span flaps. NACA-TN-1404
FRANK, JOSEPH L. Pressure-distribution and ram-recovery characteristics of NACA submerged inlets at high subsonic speeds. NACA-RM-A50E02
FRANKS, RALPH W. The application of a simplified lifting-surface theory to the prediction of the rolling effectiveness of plain spoiler ailerons at subsonic speeds. NACA-RM-A54H26A
FUCHS, RICHARD; SCHMIDT, WILHELM The steady spin. NACA-TM-630
GAINER, THOMAS G.; HOFFMAN, SHERWOOD Summary of transformation equations and equations of motion used in free flight and wind tunnel data reduction and analysis. NASA-SP-3070
GALE, LAWRENCE J. Effect of landing flaps and landing gear on the spin and recovery characteristics of airplanes. NACA-TN-1643
GARNER, I. ELIZABETH Wind-tunnel investigation of control-surface characteristics. XX - Plain and balanced flaps on an NACA 0009 rectangular semispan tail surface. NACA-WR-L-186 ; NACA-ARR-L4I11f
GILLIS, CLARENCE L.; LOCKWOOD, VERNARD E. Wind-tunnel investigation of control-surface characteristics. XIII - Various flap overhangs used with a 30-percent-chord flap on an NACA 66-009 airfoil. NACA-WR-L-314 ; NACA-ACR-3G20
GILRUTH, R. R.; TURNER, W. N. Lateral control required for satisfactory flying qualities based on flight tests of numerous airplanes. NACA-TR-715
GILRUTH, R. R.; WHITE, M. D. Analysis and prediction of longitudinal stability of airplanes. NACA-TR-711
GOETT, HARRY J.; JACKSON, ROY P.; BELSLEY, STEVEN E. Wind-tunnel procedure for determination of critical stability and control characteristics of airplanes. NACA-TR-781 ; NACA-ARR-4D29 ; NACA-WR-W-5
GOETT, HARRY J.; PASS, H. R. Effect of propeller operation on the pitching moments of single-engine monoplanes. NACA-WR-L-761
GOETT, HARRY J.; REEDER, J. P. Effects of elevator nose shape, gap, balance, and tabs on the aerodynamic characteristics of a horizontal tail surface. NACA-TR-675
GOODE, MAXWELL W.; O'BRYAN, THOMAS C.; YENNI, KENNETH R.; CANNADAY, ROBERT L.; MAYO, MARNA H. Landing practices of general aviation pilots in single-engine light airplanes. NASA-TN-D-8283
GORANSON, R. FABIAN A method for predicting the elevator deflection required to land. NACA-WR-L-95 ; NACA-ARR-L4I16
GOUGH, M. N.; BEARD, A. P. Limitations of the pilot in applying forces to airplane controls. NACA-TN-550
GRACEY, WILLIAM Measurement of Aircraft Speed and Altitude. NASA-RP-1046
GRAY, W. L.; SCHENK, K. M. A method for calculating the subsonic steady-state loading on an airplane with a wing of arbitrary plan form and stiffness. NACA-TN-3030
GREENBERG, HARRY A survey of methods for determining stability parameters of an airplane from dynamic flight measurements. NACA-TN-2340
GREENBERG, HARRY; STERNFIELD, LEONARD A theoretical investigation of the lateral oscillations of an airplane with free rudder with special reference to the effect of friction. NACA-TR-762 ; NACA-ARR-209 ; NACA-WR-L-394
GREENBERG, HARRY; STERNFIELD, LEONARD A theoretical investigation of longitudinal stability of airplanes with free controls including effect of friction in control system. NACA-TR-791 NACA-WR-L-430 NACA-ARR-4B01
GREER, H. DOUGLAS; SHIVERS, JAMES P.; FINK, MARVIN P.; CARTER, C. ROBERT Wind tunnel investigation of static longitudinal and lateral characteristics of a full scale mockup of a light single engine high wing airplane. NASA-TN-D-7149
HARRIS, THOMAS A. Reduction of hinge moments of airplane control surfaces by tabs. NACA-TR-528
HARTMAN, EDWIN P. Considerations of the take-off problem. NACA-TN-557
HOGGARD, H. PAGE ,. JR. Wind tunnel investigation of control-surface characteristics X : a 30-percent-chord plain flap with straight contour on the NACA 0015 airfoil. NACA-WR-L-366 ; NACA-ARR-121
HOGGARD, H. PAGE ,. JR. Wind-tunnel investigation of control-surface characteristics. XII - Various cover-plate alinements on the NACA 0015 airfoil with a 30-percent-chord flap and large sealed internal balance. NACA-WR-L-511
HOGGARD, H. PAGES ,. JR.; BULLOCH, MARJORIE E. Wind-tunnel investigation of control-surface characteristics. XVI - Pressure distribution over an NACA 0009 airfoil with 0.30-airfoil-chord beveled-trailing-edge flaps. NACA-WR-L-205 ; NACA-ARR-L4D03
HUNTER, P. A.; VENSEL, J. R. A flight investigation to increase the safety of a light airplane. NACA-TN-1203
HUNTER, PAUL A. Flight measurements of the flying qualities of five light airplanes. NACA-TN-1573
HUSTON, WILBER B. Accuracy of airspeed measurements and flight calibration procedures. NACA-TR-919 ; NACA-MR-L6E09 ; NACA-TN-1605
JACOBS, EASTMAN N.; ABBOTT, IRA H. Airfoil section data obtained in the N.A.C.A. variable-density tunnel as affected by support interference and other corrections. NACA-TR-669
JACOBS, EASTMAN N.; RHODE, R. V. Airfoil section characteristics as applied to the prediction of air forces and their distribution on wings. NACA-TR-631
JACOBS, EASTMAN N.; SHERMAN, ALBERT Airfoil section characteristics as affected by variations of the Reynolds number. NACA-TR-586
JACOBS, EASTMAN N.; WARD, KENNETH E.; PINKERTON, ROBERT M. The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel. NACA-TR-460
JACOBS, EASTMAN N.; WARD, KENNETH E. Interference of wing and fuselage from tests of 209 combinations in the NACA variable-density tunnel. NACA-TR-540
JEWEL, JOSEPH W. ,. JR.; MORRIS, GARLAND J. A review of the NASA V-G/VGH general aviation program. NASA-TN-D-8058
JOHNSON, HAROLD S. Wind-tunnel investigation of effects of tail length on the longitudinal and lateral stability characteristics of a single-propeller airplane model. NACA-TN-1766
JONES, ALUN R.; LEWIS, WILLIAM Recommended values of meteorological factors to be considered in the design of aircraft ice-prevention equipment. NACA-TN-1855
JONES, ROBERT T. The influence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts. NACA-TR-638
JONES, ROBERT T. Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound. NACA-TR-835 ; NACA-TN-1032 ; NACA-ACR-L5F13
JONES, ROBERT T. A simplified application of the method of operators to the calculation of disturbed motions of an airplane. NACA-TR-560
JONES, ROBERT T.; AMES, MILTON B. ,. JR. Wind-tunnel investigation of control-surface characteristics. V - The use of a beveled trailing edge to reduce the hinge moment of a control surface. NACA-WR-L-464
KATZOFF, S.; SWEBERG, HAROLD H. Ground effect on downwash angles and wake location. NACA-TR-738 ; NACA-TN-845
KAYTEN, GERALD G. Analysis of wind-tunnel stability and control tests in terms of flying qualities in full-scale airplanes. NACA-TR-825 ; NACA-WR-L-322 ; NACA-ARR-3J22
KLAWANS, BERNARD B. A simple method for calculating the characteristics of the Dutch roll motion of an airplane. NACA-TN-3754
KNIGHT, MONTGOMERY Wind tunnel tests on autorotation and the "flat spin." NACA-TR-273
LEE, DANA W. A study of the air movement in two aircraft-engine cylinders. NACA-TN-766
LEWIS, WILLIAM A flight investigation of the meteorological conditions conducive to the formation of ice on airplanes. NACA-TN-1393
LEWIS, WILLIAM; BERGRUN, NORMAN R. A probability analysis of the meteorological factors conducive to aircraft icing in the United States. NACA-TN-2738
LIDDELL, ROBERT B. Wind-tunnel investigation of control-surface characteristics. XIX - A double flap with an overhang and an internal aerodynamic balance. NACA-WR-L-215 ; NACA-ACR-L4F23
LOCKWOOD, VERNARD E. Wind-tunnel investigation of control-surface characteristics. XVII - Beveled-trailing-edge flaps of 0.20, 0.30, and 0.40 airfoil chord on an NACA 0009 airfoil. NACA-WR-L-666 ; NACA-ACR-L4D12
LOFTIN, L. K. ,. JR. Subsonic aircraft: Evolution and the matching of size to performance. NASA-RP-1060
LOWRY, JOHN G. Data on spoiler-type ailerons. NACA-RM-L53I24a
LOWRY, JOHN G. Resume of hinge-moment data for unshielded horn-balanced control surfaces. NACA-WR-L-169 ; NACA-RB-3F19
LOWRY, JOHN G.; POLHAMUS, EDWARD C. A method for predicting lift increments due to flap deflection at low angles of attack in incompressible flow. NACA-TN-3911
MALVESTUTO, FRANK S.; GALE, LAWRENCE J. Formulas for additional mass corrections to the moments of inertia of airplanes. NACA-TN-1187 ; NACA-MR-L6D03
MARTIN, G. L.; EVEREST, D. E. ,. JR.; LOVELL, W. A.; PRICE, J. E.; WALKLEY, K. B.; WASHBURN, G. F. Design and analysis of a fuel-efficient single-engine, turboprop-powered, business airplane. NASA-CR-165768
MCAVOY, W. H. Piloting technique for recovery from spins. NACA-TN-555
MCGHEE, R. J.; BEASELEY, W. D. Low-speed aerodynamic characteristics of a 17-percent-thick medium speed airfoil designed for general aviation applications. NASA-TP-1786
MCKINNEY, MARION O. ,. JR.; DRAKE, HUBERT M. Correlation of experimental and calculated effects of product of inertia on lateral stability. NACA-TN-1370
MORRIS, J. J.; SECKEL, E. Full-scale wind tunnel tests of a low-wing, single-engine, light plane with positive and negative propeller thrust and up and down flap deflection. NASA-CR-1783
MUNK, MAX M. General biplane theory. NACA-TR-151
MURRAY, HARRY E.; ERWIN, MARY A. Hinge moments of sealed-internal-balance arrangements for control surfaces. I - Theoretical investigation. NACA-WR-L-174 ; NACA-ARR-L5F30
MURRI, DANIEL G.; JORDAN, FRANK L. ,. JR. Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing. NASA-TP-2772
NEIHOUSE, A. I. The aileron as an aid to recovery from the spin. NACA-TN-776
NEIHOUSE, ANSHAL I.; KLINAR, WALTER J.; SCHER, STANLEY H. Status of spin research for recent airplane designs. NASA-TR-R-57 ; NACA-RM-L57F12
OLSON, ROLAND E.; LAND, NORMAN S. Effect of afterbody length and keel angle on minimum depth of step for landing stability and on take-off stability of a flying boat. NACA-TR-923 ; NACA-TN-1571
PASS, H. R. Analysis of wind-tunnel data on directional stability and control. NACA-TN-775
PEARSON, HENRY A.; JONES, ROBERT T. Theoretical stability and control characteristics of wings with various amounts of taper and twist. NACA-TR-635
PERSON, HENRY A.; ANDERSON, RAYMOND F. Calculation of the aerodynamic characteristics of tapered wings with partial-span flaps. NACA-TR-665
PHILLIPS, WILLIAM H. Appreciation and prediction of flying qualities. NACA-TR-927 ; NACA-TN-1670
PHILLIPS, WILLIAM H. A flight investigation of short-period longitudinal oscillations of an airplane with free elevator. NACA-WR-L-444 ; NACA-ARR-79
PHILLIPS, WILLIAM H.; KRAFT, CHRISTOPHER C. ,. JR. Theoretical study of some methods for increasing the smoothness of flight through rough air. NACA-TN-2416
PHILLIPS, WILLIAM H.; KUEHNEL, HELMUT A.; WHITTEN, JAMES B. Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes. NACA-TR-1304 ; NACA-TN-3637
PINKERTON, ROBERT M.; GREENBERG, HARRY Aerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnel. NACA-TR-628
PITTS, WILLIAM C.; NIELSEN, JACK N.; KAATTARI, GEORGE E. Lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds. NACA-TR-1307
PLATT, ROBERT C. Aerodynamic characteristics of a wing with Fowler flaps including flap loads, downwash, and calculated effect on take-off. NACA-TR-534
POVOLNY, JOHN H.; BOGDAN, LOUIS J.; CHELKO, LOUIS J. Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement. NACA-TN-2069 ; NACA-RM-E8C01
PRANDTL, L. Applications of modern hydrodynamics to aeronautics. NACA-TR-116
PURSER, PAUL E.; COOK, CHARLES B. Collection and analysis of hinge-moment data on control-surface tabs. NACA-TN-1113 ; NACA-MR-L6B14
PURSER, PAUL E.; RIEBE, JOHN M. Wind-tunnel investigation of control-surface characteristics. XV - Various contour modifications of a 0.30-airfoil-chord plain flap on an NACA 66(215)-014 airfoil. NACA-WR-L-668 ; NACA-ACR-3L20
RECANT, I. G. Plate method of ground representation for wind-tunnel determination of elevator effectiveness in landing. NACA-TN-823
RECANT, ISIDORE G.; SWANSON, ROBERT S. Determination of the stability and control characteristics of airplanes from tests of powered models. NACA-WR-L-710 ; NACA-ARR-93
RIBNER, HERBERT S. Formulas for propellers in yaw and charts of the side-force derivative. NACA-TR-819 ; NACA-ARR-3E19 ; NACA-WR-L-217
RIBNER, HERBERT S. Notes on the propeller and slipstream in relation to stability. NACA-WR-L-25 ; NACA-ARR-L4I12A
RIBNER, HERBERT S. Propellers in yaw. NACA-TR-820 ; NACA-ARR-3L09 : NACA-WR-L-219
RIBNER, HERBERT S. Proposal for a propeller side-force factor. NACA-WR-L-336 ; NACA-RB-3L02
RIBNER, HERBERT S. A transonic propeller of triangular plan form. NACA-TN-1303
RIEBE, JOHN M.; CHURCH, OLETA Wind-tunnel investigation of control-surface characteristics. XXI - Medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.40-airfoil-chord flap on an NACA 0009 airfoil. NACA-WR-L-175 ; NACA-ARR-L5C01
RIEBE, JOHN M.; MCKINNEY, ELIZABETH G. Wind-tunnel investigation of control-surface characteristics. XXII - Medium and large aerodynamic balances of two nose shapes and a plain overhang used with a 0.20-airfoil-chord flap on an NACA 0009 airfoil. NACA-WR-L-196 ; NACA-ARR-L5F06
ROGALLO, F. M. Collection of balanced-aileron test data. NACA-WR-L-419 ; NACA-ACR-4A11
SAN DIEGO AIRCRAFT ENGINEERING, INC.Potential structural materials and design concepts for light aircraft. NASA-CR-1285
SCHRENK, O., A Simple approximation method for obtaining the spanwise lift distribution. NACA-TM-948
SCHULDENFREI, MARVIN Some notes on the determination of the stick-fixed neutral point from wind-tunnel data. NACA-WR-L-344 ; NACA-RB-3I20
SEARS, RICHARD I. Wind-tunnel investigation of control-surface characteristics. I - Effect of gap on the aerodynamic characteristics of an NACA 0009 airfoil with a 30-percent-chord plain flap. NACA-WR-L-377
SEARS, RICHARD I. Wind-tunnel investigation of control-surface characteristics. IX - Some analytical considerations and experimental test results for an internally balanced flap. NACA-WR-L-339
SEARS, RICHARD I. Wind-tunnel data on the aerodynamic characteristics of airplane control surfaces. NACA-WR-L-663 ; NACA-ACR-3L08
SEARS, RICHARD I.; GILLIS, CLARENCE L. Wind-tunnel investigation of control-surface characteristics. VIII - A large aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil. NACA-WR-L-378
SEARS, RICHARD I.; HOGGARD, H. PAGE ,. JR. Wind tunnel investigation of control-surface characteristics. XI - Various large overhang and internal-type aerodynamic balances for a straight-contour flap on the NACA 0015 airfoil. NACA-WR-L-447 ; NACA-ARR-175
SEARS, RICHARD I.; HOGGARD, H. PAGE ,. JR. Wind-tunnel investigation of control-surface characteristics. II - A large aerodynamic balance of various nose shapes with a 30-percent-chord flap on an NACA 0009 airfoil. NACA-WR-L-380 ; NACA-ARR-10
SEARS, RICHARD I.; HOGGARD, H. PAGE ,. JR. Wind-tunnel investigation of control-surface characteristics. VII - A medium aerodynamic balance of two nose shapes used with a 30-percent-chord flap on an NACA 0015 airfoil. NACA-WR-L-448 ; NACA-ARR-97
SEARS, RICHARD I.; LIDDELL, ROBERT B. Wind-tunnel investigation of control-surface characteristics. VI - A 30-percent-chord plain flap on the NACA 0015 airfoil. NACA-WR-L-454
SEARS, RICHARD I.; LIDDELL, ROBERT B. Wind-tunnel investigation of control-surface characteristics. XVIII - A linked overhang aerodynamic balance. NACA-WR-L-350 ; NACA-ACR-4B28
SEARS, RICHARD I.; PURSER, PAUL E. Wind-tunnel investigation of control-surface characteristics. XIV - NACA 0009 airfoil with a 20-percent-chord double plain flap. NACA-WR-L-290 ; NACA-ARR-3F29
SHORTAL, JOSEPH A. Effect of tip shape and dihedral on lateral-stability characteristics. NACA-TR-548
SILVERSTEIN, ABE; KATZOFF, S. Aerodynamic characteristics of horizontal tail surfaces. NACA-TR-688
SILVERSTEIN, ABE; KATZOFF, S. Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings. NACA-TR-648
SILVERSTEIN, ABE; KATZOFF, S.; BULLIVANT, W. KENNETH Downwash and wake behind plain and flapped airfoils. NACA-TR-651
SIVELLS, JAMES C. Experimental and calculated characteristics of three wings of NACA 64-210 and 65-210 airfoil sections with and without 2 degree washout. NACA-TN-1422 ; NACA-L7F23a
SOMERS, D. M. Design and experimental results for a flapped natural-laminar-flow airfoil for general aviation applications. NASA-TP-1865
SOULE, HARTLEY A. Flight measurements of the dynamic longitudinal stability of several airplanes and a correlation of the measurements with pilots' observations of handling characteristics. NACA-TR-578
SPEARMAN, M. LEROY Wind-tunnel investigation of control-surface characteristics. XXIII - A 0.25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 airfoil. NACA-WR-L-47 ; NACA-ARR-L5G25
STACK, JOHN; LINDSEY, W. F.; LITTELL, ROBERT E. The compressibility burble and the effect of compressibility on pressures and forces acting on a airfoil. NACA-TR-646
STAFF OF THE FLIGHT DYNAMICS BRANCH Measurement of the handling characteristics of two light airplanes. NASA-TP-1636
STERNFIELD, LEONARD Effect of product of inertia on lateral stability. NACA-TN-1193
STERNFIELD, LEONARD Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane. NACA-TR-1042 ; NACA-TN-2233
STIVERS, LOUIS S. ,. JR. Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees. NACA-TN-3162
STONE, RALPH W. ,. JR.; HULTZ, BURTON E. Summary of spin and recovery characteristics of 12 models of flying wing and unconventional type airplanes. NACA-RM-L50L29
THEODORSEN, THEODORE General theory of aerodynamic instability and the mechanism of flutter. NACA-TR-496
THOMPSON, F. L.; GILRUTH, R. R. Notes on the stalling of vertical tail surfaces and on fin design. NACA-TN-778
TOLL, THOMAS A. ,. COMPILER Summary of lateral-control research. NACA-TR-868 ; NACA-TN-1245 ; NACA-MR-L6C22A
WEICK, FRED E.; ABRAMSON, H. NORMAN Investigation of lateral control near the stall flight tests with high-wing and low-wing monoplanes of various configurations. NACA-TN-3676
WEICK, FRED E.; ABRAMSON, H. NORMAN Investigation of lateral control near the stall. Analysis for required longitudinal trim characteristics and discussion of design variables. NACA-TN-3677
WEICK, FRED E.; JONES, ROBERT T. Resume and analysis of NACA lateral control research. NACA-TR-605
WEICK, FRED E.; SEVELSON, MAURICE S.; MCCLURE, JAMES G.; FLANAGAN, MARION D. Investigation of lateral control near the stall. Flight investigation with a light high-wing monoplane tested with various amounts of washout and various lengths of leading-edge slot. NACA-TN-2948
WEIL, JOSEPH; SLEEMAN, WILLIAM C. ,. JR. Prediction of the effects of propeller operation on the static longitudinal stability of single-engine tractor monoplanes with flaps retracted. NACA-TR-941 ; NACA-TN-1722
WEISLOGEL, G. S. Study to determine the IFR operational profile and problems of the general aviation single pilot. NASA-CR-3576
WENZINGER, CARL J.; BAMBER, MILLARD J. Wind-tunnel tests of three lateral-control devices in combination with a full-span slotted flap on an NACA 23012 airfoil. NACA-TN-659
WENZINGER, CARL J.; ROGALLO, FRANCIS M. Resume of air-load data on slats and flaps. NACA-TN-690
WHITE, MAURICE D. Estimation of stick-fixed neutral points of airplanes. NACA-WR-L-116 ; NACA-CB-L5C01
WOLOWICZ, CHESTER H.; BROWN, JAMES S. ,. JR.; GILBERT, WILLIAM P. Similitude requirements and scaling relationships as applied to model testing. NASA-TP-1435
WOLOWICZ, CHESTER H.; YANCEY, ROXANAH B. Experimental determination of airplane mass and inertial characteristics. NASA-TR-R-433
WOLOWICZ, CHESTER H.; YANCEY, ROXANAH B. Lateral-directional aerodynamic characteristics of light, twin-engine, propeller driven airplanes. NASA-TN-D-6946
WOLOWICZ, CHESTER H.; YANCEY, ROXANAH B. Longitudinal aerodynamic characteristics of light, twin-engine, propeller-driven airplanes. NASA-TN-D-6800
YIP, L. P. Wind-tunnel investigation of a full-scale canard-configured general aviation airplane. NASA-TP-2382
ZALOVCIK, JOHN A. Summary of stall-warning devices. NACA-TN-2676
ZIMMERMAN, CHARLES H. An analysis of longitudinal stability in power-off flight with charts for use in design. NACA-TR-521
ZIMMERMAN, CHARLES H. An analysis of lateral stability in power-off flight with charts for use in design. NACA-TR-589