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Primary view of Adaptation of a Cascade Impactor to Flight Measurement of Droplet Size in Clouds
Levine, Joseph & Kleinknecht, Kenneth S.
September 18, 1951
Primary view of Additional Studies of the Stability and Controllability of an Unswept-Wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques
Bates, William R.; Lovell, Powell M., Jr. & Smith, Charles C., Jr.
November 6, 1951
Primary view of The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow
Chang, Chieh-Chien
October 1951
Primary view of Aerodynamic characteristics at transonic speeds of a 69 degree delta wing with a triangular plan-form control having a skewed hinge axis and an overhang balance: transonic-bump method
Wiley, Harleth G.
February 6, 1951
Primary view of Aerodynamic characteristics including pressure distribution of a fuselage and three combinations of the fuselage with swept-back wings at high subsonic speeds
Sutton, Fred B. & Martin, Andrew
February 6, 1951
Primary view of Aerodynamic Characteristics of a Flying-Boat Hull Having a Length-Beam Ratio of 15, TED No. NACA 2206
Riebe, John M. & Naeseth, Rodger L.
January 23, 1951
Primary view of Aerodynamic characteristics of a slender cone-cylinder body of revolution at a Mach number of 3.85
Jack, John R.
November 5, 1951
Primary view of Aerodynamic Characteristics of Bodies at Supersonic Speeds: A Collection of Three Papers
Seiff, Alvin; Sandahl, Carl A.; Chapman, Dean R.; Perkins, E. W. & Gowen, F. E.
November 9, 1951
Primary view of Aerodynamic Characteristics of Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-Stream Mach Numbers From 1.50 to 1.99
Cohen, Robert J.
May 22, 1951
Primary view of Aerodynamic Characteristics of Four Wings of Sweepback Angles 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees, NACA 65A006 Airfoil Section, Aspect Ratio 4, and Taper Ratio 0.6 in Combination With a Fuselage at High Subsonic Mach Numbers and at a Mach Number of 1.2
Luoma, Arvo A.
June 6, 1951
Primary view of Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-Chord Lines Swept Back 45 Degrees, and NACA 63(Sub 1)a012 Airfoil Sections: Transonic-Bump Method
Polhamus, Edward C. & King, Thomas J., Jr.
June 13, 1951
Primary view of Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98
Perkins, Edward W.; Gowen, Forrest E. & Jorgensen, Leland H.
September 19, 1951
Primary view of Aerodynamic Characteristics of Wings Designed for Structural Improvement
Weil, Joseph & Polhamus, Edward C.
May 28, 1951
Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness at supersonic speeds of a 30-percent chord, 50-percent semispan elevon as a lateral control device
Olson, Robert N. & Mead, Merrill H.
January 18, 1951
Primary view of Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) 1: body of revolution with near-parabolic forebody and cylindrical afterbody
Jack, John R. & Burgess, Warren C.
November 13, 1951
Primary view of Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow
Watkins, Charles E.
September 1951
Primary view of Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow
Watkins, Charles E. & Berman, Julian H.
June 19, 1951
Primary view of Altitude-ignition limit of a turbojet engine using a condenser-discharge ignition system
Armstrong, John C.
October 23, 1951
Primary view of Altitude investigation of 16 flame-holder and fuel-system configurations in tail-pipe burner
Grey, Ralph E.; Krull, H. G. & Sargent, A. F.
December 12, 1951
Primary view of Altitude Operation of Gas-Turbine Engine With Variable-Area Fuel-Nozzle System
Gold, H. & Rosenzweig, S.
April 2, 1951
Primary view of Altitude-performance and Reynolds number investigation of centrifugal-flow-compressor turbojet engine
Wilsted, H. D. & Grey, R. E.
May 15, 1951
Primary view of Altitude Performance of J35-A-17 Turbojet Engine in an Altitude Chamber
Vincent, K. R. & Gale, B. M.
January 3, 1951
Primary view of Altitude-test-chamber investigation of performance of a 28-inch ram-jet engine 3: combustion and operational performance of three flame holders with a center pilot burner
Shillito, Thomas B.; Younger, George G. & Henzel, James G., Jr.
February 6, 1951
Primary view of Altitude-Test-Chamber Investigation of Performance of a 28-Inch Ram-Jet Engine 4: Effect of Inlet-Air Temperature, Combustion-Chamber-Inlet Mach Number, and Fuel Volatility on Combustion Performance
Kahn, Robert W.; Nakanishi, Shigeo & Harp, James L., Jr.
July 27, 1951
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