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Primary view of Impingement of water droplets on an NACA 65(sub 1) -212 airfoil at an angle of attack of 4 degrees
Brun, Rinaldo J.; Serafini, John S. & Moshos, George J.
September 10, 1952
Primary view of Investigation of Spinning and Tumbling Characteristics of a 1/20-Scale Model of the Consolidated Vultee XFY-1 Airplane in the Free-Spinning Tunnel, TED No. NACA DE 370
Lee, Henry A.
December 10, 1952
Primary view of Tank Investigation of the Grumman JRF-5 Airplane Equipped with Twin Hydro-Skis: TED No. NACA DE 357
Ramsen, John A. & Gray, George R.
April 10, 1952
Primary view of Investigation in the Ames Supersonic Free-Flight Wind Tunnel of the Static Longitudinal Stability of the Hermes A-3B Missile at a Mach Number of 5.0
Canning, Thomas N. & Denardo, Billy Pat
March 10, 1952
Primary view of Preliminary investigation of control characteristics at transonic speeds of a tapered 45 degree sweptback wing of aspect ratio 3 having a horn-balanced full-span control
Lowry, John G. & Fikes, Joseph E.
April 10, 1952
Primary view of Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Twisted and cambered triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution
Heitmeyer, John C. & Petersen, Robert B.
April 10, 1952
Primary view of Component and over-all performance evaluation of an axial-flow turbojet engine over a range of engine-inlet Reynolds numbers
Walker, Curtis L.; Huntley, S. C. & Braithwaite, W. M.
July 10, 1952
Primary view of Investigation at Mach Number 2.93 of Half of a Conical-Spike Diffuser Mounted as a Side Inlet With Boundary-Layer Control
Piercy, Thomas G. & Johnson, Harry W.
September 10, 1952
Primary view of Altitude investigation of three flame-holder and fuel-systems configurations in a short converging afterburner on a turbojet engine
Braithwaite, Willis M.; Renas, Paul E. & Jansen, Emmert T.
September 10, 1952
Primary view of Effect of trailing edge thickness on lift at supersonic velocities
Chapman, Dean R. & Kester, Robert H.
July 10, 1952
Primary view of Investigation of vanes immersed in the jet of a solid-fuel rocket motor
Giladett, Leo V. & Wineman, Andrew R.
September 10, 1952
Primary view of Survey of some preliminary investigations of supersonic diffusers at high Mach numbers
Cortright, Edgar M., Jr. & Connors, James F.
July 10, 1952
Primary view of Solubility of water in hydrocarbons
Hibbard, R. R. & Schalla, R. L.
July 10, 1952
Primary view of Low-Speed Lateral-Control Investigation of a Flap-Type Spoiler Aileron With and Without a Deflector and Slot on a 6-Percent-Thick, Tapered, 45 Degree Sweptback Wing of Aspect Ratio 4
Watson, James M.
September 10, 1952
Primary view of An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degrees Sweepback: Estimated Downwash Angles Derived From Pressure Measurements on the Tail at Mach Numbers of 1.40 and 1.59
Grant, Frederick C. & Gapcynski, John P.
March 10, 1952
Primary view of Experimental investigation of an axial flow compressor inlet stage operating at transonic relative inlet Mach numbers 1: over-all performance of stage with transonic rotor and subsonic stators up to rotor relative inlet Mach number of 1.1
Lieblein, Seymour; Lewis, George W., Jr. & Sandercock, Donald M.
March 10, 1952
Primary view of Low-speed investigation of the effects of wing leading-edge modifications and several outboard fin arrangements on the static stability characteristics of a large-scale triangular wing
McLemore, H. Clyde
January 10, 1952
Primary view of Small-scale transonic investigation of the effects of twist and camber on the aerodynamic characteristics of a 60 degrees 42' sweptback wing of aspect ratio 1.94
Spreemann, Kenneth P. & Alford, William J., Jr.
January 10, 1952
Primary view of Studies of the flow field behind a large scale 47.5 degree sweptback wing having circular-arc airfoil sections and equipped with drooped-nose and plain flaps
Lange, Roy H. & Fink, Marvin P.
March 10, 1952
Primary view of An Investigation of Propeller Vibrations Excited by Wing Wakes
Gray, W. H. & Solomon, William
January 10, 1952
Primary view of Hydrodynamic Directional Behavior of a Swept Planing-Tail Hull
Arabian, Donald D.
January 10, 1952
Primary view of An Analysis of the Effect of Structural Feedback on the Flutter of a Control Surface Having a Power-Boost System
Barnes, Robert H.
June 10, 1952
Primary view of Facilities and methods used in full-scale airplane crash-fire investigation
Black, Dugald O.
March 10, 1952
Primary view of Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2: Effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch
Robinson, Ross B. & Driver, Cornelius
January 10, 1952
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