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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 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 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
Primary view of Altitude-Wind-Tunnel Investigation of Performance Characteristics of a J47D Prototype (RX1-1) Turbojet Engine With Fixed-Area Exhaust Nozzle
Saari, M. J. & Wintler, J. T.
September 4, 1951
Primary view of Altitude-Wind-Tunnel Investigation of Performance Characteristics of a J47D Prototype (RX1-1) Turbojet Engine With Variable-Area Exhaust Nozzle
Conrad, E. William & McAulay, John E.
September 5, 1951
Primary view of Altitude Wind Tunnel Investigation of the Performance of Compressor, Combustor, and Turbine Components of Prototype J47D (RX1-1) Turbojet Engine
Farley, John M.
December 21, 1951
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