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ABOUT BROWSE FEED
Primary view of Performance of a Single Fuel-vaporizing Combustor With Six Injectors Adapted for Gaseous Hydrogen
Smith, A. L. & Wear, J. D.
November 30, 1959
Primary view of Some Research on the Lift and Stability of Wing-Body Combinations
Purser, Paul E. & Fields, E. M.
July 2, 1959
Primary view of Preliminary analysis of hydrogen-rich hypersonic ramjet operation
Breitwieser, R. & Morris, J. F.
May 29, 1959
Primary view of An analytical evaluation of the effects of an aerodynamic modification and of stability augmenters on the pitch behavior and probable pilot opinion of two current fighter airplanes
Sadoff, Melvin & Stewart, John D
April 21, 1959
Primary view of Effects of components and various modifications on the drag and the static stability and control characteristics of a 42 deg swept-wing fighter-airplane model at Mach numbers of 1.60 to 2.50
Church, J. D.
April 15, 1959
Primary view of Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine
Heidmann, M F & Baker, Louis, Jr
September 30, 1958
Primary view of Off-Design Performance of Divergent Ejectors
Beheim, M. A.
September 30, 1958
Primary view of Off-design performance of divergent ejectors
Beheim, Milton A
September 30, 1958
Primary view of Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8
Martz, C William
September 30, 1958
Primary view of Screaming tendency of the gaseous-hydrogen - liquid-oxygen propellant combination
Baker, Louis, Jr & Steffen, Fred W
September 30, 1958
Primary view of Use of highly reactive chemical additives to improve afterburner performance at altitude
Sivo, J. N. & Wanhainen, J. P.
September 30, 1958
Primary view of Use of highly reactive chemical additives to improve afterburner performance at altitude
Wanhainen, John P. & Sivo, Joseph N.
September 30, 1958
Primary view of Some notes on the probable damage to an intercontinental-ballistic-missile warhead following puncture of the heat shield
Strass, H. K. & Goodman, V. M.
September 28, 1958
Primary view of Analysis of pressure data obtained at transonic speeds on a thin low-aspect-ratio cambered delta wing-body combination
Mugler, John P , Jr
September 26, 1958
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 Large-scale wind-tunnel tests of a jet-transport-type model with leading- and trailing-edge high-lift devices
Aoyagi, Kiyoshi & Hickey, David H
September 26, 1958
Primary view of Static and dynamic-rotary stability derivatives of an airplane model with an unswept wing and a high horizontal tail at Mach numbers of 2.5, 3.0, and 3.5
Lampkin, Bedford A & Tunnell, Phillips J
September 26, 1958
Primary view of Effect of spike-tip and cowl-lip blunting on inlet performance of a Mach 3.0 external-compression inlet
Cubbison, R W & Samanich, N E
September 23, 1958
Primary view of Effect of spike-tip and cowl-lip blunting on inlet performance of a Mach 3.0 external- compression inlet
Cubbison, R. N. & Samanich, N. E.
September 23, 1958
Primary view of Experimental investigation of effect of spike- tip and cowl-lip blunting on the internal performance of a two-cone cylindrical-cowl inlet at mach number 4.95
Weston, K. C.
September 23, 1958
Primary view of Experimental Study of Ballistic-Missile Base Heating with Operating Rocket
Nettle, J. Cary
September 23, 1958
Primary view of Investigation of Inlet Control Parameters for an External-Internal-Compression Inlet from Mach 2.1 to 3.0
Anderson, B. H. & Bowditch, D. N.
September 23, 1958
Primary view of A Flight Study of the Effects of Noise Filtering in the Attack Display on the Pilot's Tracking Performance
Heinle, D. R. & Turner, H. L.
September 20, 1958
Primary view of Aerodynamic performance and static stability and control of flat-top hypersonic gliders at Mach numbers from 0.6 to 18
Syvertson, Clarence A; Gloria, Hermilo R & Sarabia, Michael F
September 17, 1958