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Primary view of Transonic Wind-Tunnel Tests of the Launch, Jettison, and Longitudinal Characteristics of an Airplane and Missile Model Combination
Cleary, Joseph W.; Frank, Joseph L. & Dewey, C. Forbes, Jr.
November 20, 1957
Primary view of Theoretical Analysis of the Interference Effects of Several Supersonic Tunnel Walls Capable of Absorbing the Shock Caused by the Nose of a Model
Matthews, Clarence W.
May 26, 1958
Primary view of Some Effects of Aileron Deflection on the Static Lateral and Directional Aerodynamic Characteristics of Four Contemporary Airplane Models
Smith, Willard G. & Intrieri, Peter F.
July 23, 1957
Primary view of Preliminary Analysis of a Nuclear Powered Supersonic Airplane Using Ramjet Engines
Weber, Richard J. & Connolley, Donald J.
April 11, 1958
Primary view of Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Turbine Failure Investigation of J65-W-4 Turbojet Engine in an Altitude Test Chamber
McAulay, John E.; Braithwaite, Willis M. & Ciepluch, Carl C.
September 21, 1956
Primary view of Free Flight Investigation at Transonic Speeds of the Power-on Characteristics Including Some Effects of Sonic Propulsive Jets of a Four Engine Delta Wing Configuration
Falanga, Ralph A. & Judd, Joseph H.
August 16, 1957
Primary view of Hydrodynamic Characteristics of Missiles Launched Under Water
Dawson, John R.
June 27, 1958
Primary view of A Preliminary Investigation of the Performance of a Short Length Turbojet Combustor Using Vaporized Hydrocarbon Fuels
Jones, R. E. & Pawlik, E. V.
January 7, 1958
Primary view of Heat-Exchanger-Core Weights for Use With Hydrogen-Expansion Turbine
Reynolds, Thaine W.
October 3, 1957
Primary view of Altitude chamber evaluation of an aircraft liquid hydrogen fuel system used with a turbojet engine
Braithwaite, Willis M.; Fenn, David B. & Algranti, Joseph S.
August 19, 1957
Primary view of Hydrogen for Turbojet and Ramjet Powered Flight
Lewis Flight Propulsion Laboratory
April 26, 1957
Primary view of High Altitude Performance Investigation of J65-B-3 Turbojet Engine With Both JP-4 and Gaseous Hydrogen Fuels
Kaufman, Harold R.
April 2, 1957
Primary view of Analysis of turbojet and ram-jet engine cycles using various fuels
Wilcox, E. Clinton; Weber, Richard J. & Tower, Leonard K.
November 27, 1956
Primary view of Experimental Investigation of Diffuser Pressure Ratio Control With Shock Positioning Limit on 28 Inch Ram-Jet Engine
Dunbar, William R.; Wentworth, Carl B. & Crowl, Robert J.
January 15, 1957
Primary view of Experimental Evaluation of Swirl Can Elements for Hydrogen Fuel Combustor
Rayle, Warren D.; Jones, Robert E. & Friedman, Robert
May 13, 1957
Primary view of Design and performance of flight-type liquid-hydrogen heat exchanger
Fenn, David B.; Braithwaite, Willis M. & Ordin, Paul M.
August 19, 1957
Primary view of Design and Performance of Fuel Control for Aircraft Hydrogen Fuel System
Otto, Edward W.; Hiller, Kirby W. & Ross, Phil S.
August 19, 1957
Primary view of Flight Investigation of a Liquid Hydrogen Fuel System
Mulholland, Donald R.; Acker, Loren W.; Christenson, Harold H. & Gough, William V.
August 19, 1957
Primary view of Wind-Tunnel Investigation of a 1/60-Scale Model of the Republic MX-1554 Airplane at a Mach Number of 2.85
Dickey, Robert R. & Spahr, J. Richard
March 18, 1953
Primary view of Tracking Performance of a Swept-Wing Fighter With a Director-Type Radar Fire-Control System and Scope Presentation
Turner, Horward L.; Rathert, George A., Jr. & Heinle, Donovan R.
January 20, 1958
Primary view of A Flight Study of the Effects of Noise Filtering in the Attack Display on the Pilot's Tracking Performance
Turner, Howard L. & Heinle, Donovan R.
September 10, 1958
Primary view of Thrust and Pumping Characteristics of a Series of Ejector-type Exhaust Nozzles at Subsonic and Supersonic Flight Speeds
Hearth, Donald P. & Valerino, Alfred S.
November 17, 1954
Primary view of Analysis of Limitations Imposed on One-Spool Turbojet-Engine Designs by Turbines Having Downstream Stators at 0, 2.0, and 2.8 Flight Mach Numbers
Cavicchi, Richard H. & Constantine, Anita B.
January 19, 1955
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