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Primary view of Analysis of the High-Altitude Cooling of the Ranger SGV-770 D-4 Engine in the Bell XP-77 Airplane
Nielsen, Jack N. & Schumacher, Lloyd E.
October 1943
Primary view of Annual Report of the National Advisory Committee for Aeronautics (42nd), Administrative Report without Technical Reports
unknown creator
October 17, 1956
Primary view of N.A.C.A. control position recorder
Norton, F. H.
May 1922
Primary view of Investigation of Wingless Missile Configurations with Folding Controls and Low-Aspect-Ratio Stabilizing Surfaces
Lazzeroni, Frank A.
September 17, 1958
Primary view of Preliminary Results from Free-Jet Tests of a 48-Inch-Diameter Ram-Jet Combustor with an Annular-Piloted Baffle-Type Flameholder
Rayle, W. D.; Smith, I. D. & Wentworth, C. B.
May 11, 1955
Primary view of Preliminary Data on Rain Deflection from Aircraft Windshields by Means of High-Velocity Jet-Air Blast
Ruggeri, Robert S.
July 25, 1955
Primary view of Flight Instrument for Measurement of Liquid-Water Content in Clouds at Temperatures Above and Below Freezing
Perkins, Porter J.
March 5, 1951
Primary view of Impingement of Water Droplets on an NACA 65(sub 1) -212 Airfoil at an Angle of Attack of 4 Deg
Brun, Rinaldo J.; Serafini, John S. & Moshos, George J.
September 10, 1952
Primary view of Investigation of Porous Gas-Heated Leading-Edge Section for Icing Protection of a Delta Wing
Bowden, Dean T.
January 19, 1955
Primary view of Tracking Performance of a Swept-wing Fighter With a Directortype Radar Fire-control System and Scope Presentation
Heinle, D. R.; Rathert, G. A. & Turner, H. L.
January 20, 1958
Primary view of Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-aspect-ratio Swept-back Wing-stability and Control
Smith, W. G.
January 12, 1953
Primary view of Wind-tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept-wing Airplane With Blowing Flaps and Leading-edge Slats
James, H. A. & Maki, R. L.
April 5, 1957
Primary view of Wing-body combinations with wings of very low aspect ratio at supersonic speeds
Jorgensen, L. H. & Katzen, E. D.
October 26, 1956
Primary view of Boundary-Layer-Transition Measurements in Full-Scale Flight
Banner, Richard D.; McTigue, John G. & Petty, Gilbert, Jr.
July 28, 1958
Primary view of Pressure Distributions and Aerodynamic Characteristics of Several Spoiler-type Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01
Czarnecki, K. R. & Lord, D. R.
July 26, 1956
Primary view of Analysis of flight-determined and predicted effects of flexibility on the steady-state wing loads of the B-52 airplane
Kuhl, A. E.; Little, M. V. & Rogers, J. T.
April 23, 1958
Primary view of Induction system characteristics and engine surge occurrence for two fighter-type airplanes
Bellman, D. R.; Larson, T. J. & Thomas, G. M.
May 26, 1958
Primary view of In-flight Gains Realized by Modifying a Twin Side-inlet Induction System
Saltzman, E. J.
December 12, 1957
Primary view of Heat Transfer Measured in Free Flight on a Slightly Blunted 25 deg Cone-Cylinder-Flare Configuration at Mach Numbers up to 9.89
Bond, Aleck C.; Lee, Dorothy B. & Rumsey, Charles B.
September 26, 1958
Primary view of Model ditching investigations of three airplanes equipped with hydro-skis
Fisher, L. J.
April 25, 1950
Primary view of A note on the ability to predict transonic drag-rise changes due to model modifications
Pierpont, P. K.
October 3, 1957
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselage-store Configurations. Ii - Swept-wing Heavy-bomber Configuration With Large Store Nacelle . Lateral Forces and Pitching Moments, Mach Number, 1.61
Carlson, H. W. & Smith, N. F.
July 6, 1955
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselagestore Configurations. 1.-swept-wing Heavy-bomber Configuration With Large Store Nacelle . Lift and Drag, Mach Number, 1.61
Carlson, H. W. & Smith, N. F.
March 11, 1955
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselagestore Configurations. Iii - Swept-wing Fighter-bomber Configuration With Large and Small Stores. Mach Number, 1.61
Carlson, H. W. & Smith, N. F.
September 15, 1955