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Primary view of Ditching Investigation of a 1/18-Scale Model of the North American B-45 Airplane
Fisher, Lloyd J. & Thompson, William C.
December 22, 1949
Primary view of Flight Test of the Aerojet 7KS-6000 T-27 Jato Rocket Motor
Bond, Aleck C. & Thibodaux, Joseph G., Jr.
December 20, 1949
Primary view of A Free-Flight Technique for Measuring Damping in Roll by Use of Rocket-Powered Models and Some Initial Results for Rectangular Wings
Edmondson, James L. & Sanders, E. Claude, Jr.
December 20, 1949
Primary view of Comparison of Effectiveness of Coordinated Turns and Level Sideslips for Correcting Lateral Displacement During Landing Approaches
Faber, Stanley
December 15, 1949
Primary view of Low-Speed Investigation of Deflectable Wing-Tip Ailerons on an Untapered 45 Degrees Sweptback Semispan Wing With and Without an End Plate
Fischel, Jack & Watson, James M.
December 14, 1949
Primary view of Preliminary Investigation of a Variable Mass-Flow Supersonic Nose Inlet
Hayes, Clyde
December 13, 1949
Primary view of Comparative Tests of the Rolling Effectiveness of Constant-Chord, Full-Delta, and Half-Delta Ailerons on Delta Wings at Transonic and Supersonic Speeds
Sandahl, Carl A. & Strass, H. Kurt
December 12, 1949
Primary view of Experimental investigation at supersonic speeds of side scoops employing boundary-layer suction
Edwards, Sherman S.
December 12, 1949
Primary view of The effects of scale and test technique on the validity of small-scale measurements of the aerodynamic characteristics of a wing with the leading edge swept back 63 degrees
Rolls, L. Stewart
December 9, 1949
Primary view of An empirical criterion for fin stabilizing jettisonable nose sections of airplanes
Scher, Stanley H.
December 8, 1949
Primary view of Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-Foot Pressure Wind Tunnel 5: Static Longitudinal Stability and Control Throughout the Subsonic Speed Range of a Semispan Model of a Supersonic Airplane
Johnson, Ben H., Jr. & Rollins, Francis W.
December 8, 1949
Primary view of Full-Scale Hydrodynamic Evaluation of a Modified Navy J4F-2 Amphibian with a 0.425-Scale XP5M-1 Hull Bottom: TED No. NACA DE325
Land, Norman S.; Elliott, John M. & Christopher, Kenneth W.
December 7, 1949
Primary view of Aerodynamic Study of a Wing-Fuselage Combination Employing a Wing Swept Back 63 Degrees: Effects at Subsonic Speeds of a Constant-Chord Elevon on a Wing Cambered and Twisted for a Uniform Load at a Lift Coefficient of 0.25
Jones, J. Lloyd & Demele, Fred A.
December 5, 1949
Primary view of Investigation of altitude performance of AN-F-58 fuels in annular combustor of J34-WE-22 engine
Tischler, Adelbert O. & Scull, Wilfred E.
December 5, 1949
Primary view of Survey of two-dimensional data on pitching-moment changes near maximum lift caused by deflection of high-lift devices
Bidwell, Jerold M. & Cahill, Jones F.
December 2, 1949
Primary view of Effect of airfoil section and tip tanks on the aerodynamic characteristics at high subsonic speeds of an unswept wing of aspect ratio 5.16 and taper ratio 0.61
Silvers, H. Norman & Spreeman, Kenneth P.
December 1, 1949
Primary view of Flight Investigations at High-Subsonic, Transonic, and Supersonic Speeds to Determine Zero-Lift Drag of Fin-Stabilized Bodies of Revolution having Fineness Ratios of 12.5, 8.91, and 6.04 and Varying Positions of Maximum Diameter
Hart, Roger G. & Katz, Ellis R.
November 30, 1949
Primary view of Spin-Tunnel Investigation of the Jettisoning of External Fuel Tanks in Spins
Berman, Theodore
November 30, 1949
Primary view of Wing-tunnel investigation at low transonic speeds of the effects of number of wings on the lateral-control effectiveness of an RM-5 test vehicle
Johnson, Harold S.
November 29, 1949
Primary view of Altitude-wind-tunnel investigation of compressor performance on J47 turbojet engine
Prince, William R. & Jansen, Emmert T.
November 22, 1949
Primary view of Low-speed pressure-distribution and flow investigation for a large pitch and yaw range of three low-aspect-ratio pointed wings having leading edge swept back 60 degrees and biconvex sections
May, Ralph W., Jr. & Hawes, John G.
November 18, 1949
Primary view of Performance of Axial-Flow Supersonic Compressor of the XJ55-FF-1 Turbojet Engine. 4 - Analysis of Compressor Operation over a Range of Equivalent Tip Speeds from 801 to 1614 Feet Per Second
Graham, Robert C. & Hartmann, Melvin J.
November 18, 1949
Primary view of Study of the canard configuration with particular reference to transonic flight characteristics and low-speed characteristics at high lift
Mathews, Charles W.
November 16, 1949
Primary view of Altitude-wind-tunnel investigation of J47 turbojet-engine performance
Conrad, E. William & Sobolewski, Adam E.
November 15, 1949
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