UNT Libraries Government Documents Department - 5,163 Matching Results

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Primary view of An 8-foot axisymmetrical fixed nozzle for subsonic Mach numbers up to 0.99 and for a supersonic Mach number of 1.2
Ritchie, Virgil S.; Wright, Ray H. & Tulin, Marshall P.
February 23, 1950
Primary view of Ability of pilots to control simulated short-period yawing oscillations
Phillips, William H & Cheatham, Donald C
November 13, 1950
Primary view of Abstracts pertaining to seaplanes
Bidwell, Jerold M & King, Douglas A
July 24, 1947
Primary view of Acceleration characteristics of a turbojet engine with variable-position inlet guide vanes
Dobson, W F & Wallner, Lewis E
July 7, 1955
Primary view of Acceleration Characteristics of R-3350 Engine Equipped with NACA Injection Impeller
Hickel, Robert O. & Snider, William E.
January 8, 1947
Primary view of Acceleration Measurements During Landing in Rough Water of a 1/7-Scale Dynamic Model of Grumman XJR2F-1 Amphibian - Langley Tank Model 212, TED No. NACA 2378
Land, Norman S. & Zeck, Howard
May 6, 1947
Primary view of Acceleration Measurements During Landings of a 1/5.5-Size Dynamic Model of the Columbia XJL-1 Amphibian in Smooth Water and in Waves: Langley Tank Model 208M, TED No. NACA 2336
Clement, Eugene P. & Havens, Robert F.
September 25, 1947
Primary view of Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics : effect of compressor interstage air bleed
Rebeske, John J , Jr & Dugan, James F , Jr
July 3, 1953
Primary view of Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics I : effect of air bleed at compressor outlet
Rebeske, John J , Jr & Rohlik, Harold E
March 10, 1953
Primary view of Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics III : effect of turbine stator adjustment
Rohlik, Harold E & Rebeske, John J
August 2, 1954
Primary view of An acceleration schedule control for accelerating a turbojet engine and its use with a speed control
Gerus, Theodore F; Powers, Albert G & Heppler, Herbert J
May 12, 1958
Primary view of An acceleration schedule control for accelerating a turbojet engine and its use with a speed control
Gerus, T. F.; Heppler, H. J. & Powers, A. G.
May 12, 1958
Primary view of Accelerations in fighter-airplane crashes
Acker, Loren W; Black, Duglad O & Moser, Jacob C
November 4, 1957
Primary view of An active particle diffusion theory of flame quenching for laminar flames / Dorothy M. Simon and Frank E. Belles
Simon, Dorothy M & Belles, Frank E
March 4, 1952
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 Adaptation of Combustion Principles to Aircraft Propulsion, Volume 1, Basic Considerations in the Combustion of Hydrocarbon Fuels with Air
Barnett, Henry C. & Hibbard, Robert R.
April 1, 1955
Primary view of Adaptation of Combustion Principles to Aircraft Propulsion, Volume 2, Combustion in Air-Breathing Jet Engines
unknown creator
May 2, 1956
Primary view of Additional abstracts pertaining to seaplanes
Bidwell, J. M. & King, D. A.
March 9, 1948
Primary view of Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations
Holdaway, George H
August 15, 1955
Primary view of Additional experimental heat-transfer and durability data on several forced-convection, air-cooled, strut-supported turbine blades of improved design
Schum, Eugene F
January 19, 1955
Primary view of Additional experiments with flat-top wing- body combinations at high supersonic speeds
Gloria, H. R.; Syvertson, C. A. & Wong, T. J.
February 19, 1957
Primary view of Additional fatigue tests on effects of design details in 355-T6 sand-cast aluminum alloy
Eaton, I D & Youra, John A
March 10, 1954
Primary view of Additional free-flight tests of the rolling effectiveness of several wing-spoiler arrangements at high subsonic, transonic, and supersonic speeds
Strass, H Kurt
November 24, 1948
Primary view of Additional measurements of the low-speed static stability of a configuration employing three triangular wing panels and a body of equal length
Delany, Noel K
July 25, 1955