UNT Libraries Government Documents Department - 22 Matching Results

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Primary view of Altitude performance of J71-A-2(600-D1) turbojet engine
Smith, Ivan D. & Sivo, Joseph N.
December 28, 1956
Primary view of Attenuation of Tangential-Pressure Oscillations in a Liquid-Oxygen-n-Heptane Rocket Engine With Longitudinal Fins
Priem, Richard J.
June 28, 1956
Primary view of Attenuation of tangential-pressure oscillations in a liquid-oxygen - n-heptane rocket engine with longitudinal fins
Priem, Richard J.
June 28, 1956
Primary view of A Bibliography of NACA Reports on Control of Turbojet Engines
Sanders, John C.
June 28, 1956
Primary view of Component performance of J71-A-2(600-D1) turbojet engine at several Reynolds number indices
Seashore, Ferris L. & Corrington, Lester C.
December 28, 1956
Primary view of Effect of a Fuselage on the Low-Speed Longitudinal Aerodynamic Characteristics of a 45 Degree Sweptback Wing with Double Slotted Flaps
Naeseth, Rodger L.
September 28, 1956
Primary view of Evaluation of Liquefied Hydrocarbon Gases as Turbojet Fuels
Hibbard, Robert R.
December 28, 1956
Primary view of Experimental and analytical investigation of an acceleration regulating control for a turbojet engine
Stiglic, Paul M.; Heppler, Herbert & Novik, David
June 28, 1956
Primary view of Experimental Investigation of a Transonic Axial-Flow-Compressor Rotor Designed for Sonic Inlet Velocity with an Inlet Hub-Tip Radius of 0.35
Boxer, Emanuel & Bernot, Peter T.
September 28, 1956
Primary view of Free-flight Investigation at Transonic Speeds of the Stability Characteristics of a Tailless Missile Configuration Having a 45 Deg Sweptback Wing of Aspect Ratio 4
Arbic, Richard G.
August 28, 1956
Primary view of Free-Flight Investigation at Transonic Speeds of the Stability Characteristics of a Tailless Missile Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 4
Arbic, Richard G.
August 28, 1956
Primary view of Free-flight investigation over a Mach number range from 0.74 to 1.43 at lift coefficients from minus 0.15 to 0.75 of an airplane-configuration model having a 52.5 degree delta wing and a low swept horizontal tail
Kehlet, Alan B.
September 28, 1956
Primary view of Full-Scale Evaluation of Some Flameholder Design Concepts for High-Inlet-Velocity Afterburners
Prince, William R.; Velie, Wallace W. & Braithwaite, Willis M.
June 28, 1956
Primary view of Full-scale evaluation of some flameholder design concepts for high-inlet-velocity afterburners
Prince, William R.; Velie, Wallace W. & Braithwaite, Willis M.
June 28, 1956
Primary view of Hinge Moment and Effectiveness of an Unswept Constant-Chord Control and an Overhang-Balanced, Swept Hinge-Line Control on an 80 Degree Swept Pointed Wing at Mach Numbers from 0.75 to 1.96
Guy, Lawrence D.
August 28, 1956
Primary view of Longitudinal and Lateral Stability Characteristics of a Low-Aspect-Ratio Unswept-Wing Airplane Model at Mach Numbers of 1.82 and 2.01
Spearman, M. Leroy & Driver, Cornelius
January 28, 1956
Primary view of Performance of a blunt-lip side inlet with ramp bleed, bypass, and a long constant-area duct ahead of the engine : Mach number 0.66 and 1.5 to 2.1
Allen, John L.
December 28, 1956
Primary view of Performance of a Blunt-lip Side Inlet With Ramp Bleed, Bypass, and a Long Constant-area Duct Ahead of the Engine- Mach Numbers 0.66 and 1.5 to 2.1
Allen, John L.
December 28, 1956
Primary view of Stability of supersonic inlets at Mach 1.91 with air injection and suction
Kowalski, K. & Piercy, Thomas G.
June 28, 1956
Primary view of Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration
Gillespie, Warren, Jr.
September 28, 1956
Primary view of Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration
Gillespie, Warren, Jr.
September 28, 1956
Primary view of Wind-Tunnel Investigation of the Interference Effects during Separation of a 1/40-Scale Model Convair B-58 Airplane and Store at Mach Numbers of 1.41, 1.61, and 2.01
Driver, Cornelius
December 28, 1956
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