UNT Libraries Government Documents Department - 231 Matching Results

Search Results

Results: 1 - 24 next
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 Aerodynamic characteristics at transonic speeds of a wing having a 45 degree sweep, aspect ratio 8, taper ratio 0.45, and airfoil sections varying from the NACA 63A010 section at the root to the NACA 63A006 section at the tip.
Morrison, William D., Jr. & Fournier, Paul G.
January 15, 1952
Primary view of Aerodynamic Loads on an External Store Adjacent to a 45 Degree Sweptback Wing at Mach Numbers From 0.70 to 1.96, Including an Evaluation of Techniques Used
Guy, Lawrence D. & Hadaway, William M.
November 15, 1955
Primary view of Aerodynamic Study of a Wing-Fuselage Combination Employing a Wing Swept Back 63 Degrees: Characteristics Throughout the Subsonic Speed Range With the Wing Cambered and Twisted for a Uniform Load at a Lift Coefficient of 0.25
Jones, J. Lloyd & Demele, Fred A.
August 15, 1949
Primary view of Aircraft Accidents: Method of Analysis
Special Committee on the Nomenclature, Subdivision, and Classification of Aircraft Accidents
August 15, 1928
Primary view of Altitude Free-Jet Investigation of Dynamics of a 28-Inch-Diameter Ram-Jet Engine
Wentworth, Carl B.; Dunbar, William R. & Crowl, Robert J.
January 15, 1957
Primary view of Altitude-performance and Reynolds number investigation of centrifugal-flow-compressor turbojet engine
Wilsted, H. D. & Grey, R. E.
May 15, 1951
Primary view of Altitude Performance of a 20-Inch-Diameter Ram-Jet Engine Investigated in a Free-Jet Facility at Mach Number 3.0
Smolak, George R. & Wentworth, Carl B.
June 15, 1953
Primary view of Altitude Performance of a 20-Inch-Diameter Ram-Jet Engine Investigated in a Free Jet Facility at Mach Number 3.0
Smolak, George R. & Wentworth, Carl B.
June 15, 1953
Primary view of Altitude performance of compressor, turbine, and combustor components of 600-B9 turbojet engine
Prince, William R. & Wile, Dorwin B.
March 15, 1954
Primary view of Altitude-Wind-Tunnel Investigation of Combustion-Chamber Performance on J47 Turbojet Engine
Campbell, Carl E.
December 15, 1950
Primary view of Altitude-wind-tunnel investigation of J47 turbojet-engine performance
Conrad, E. William & Sobolewski, Adam E.
November 15, 1949
Primary view of Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine IV: performance with tail-pipe burning and water injection
Dietz, Robert O., Jr.; Wishnek, George & Kuenzig, John K.
June 15, 1948
Primary view of Analysis of the Effects of Various Mass, Aerodynamic, and Dimensional Parameters on the Dynamic Lateral Stability of the Douglas D-558-2 Airplane
Queijo, M. J. & Michael, W. H., Jr.
April 15, 1949
Primary view of An Analysis of the Stability of an Airplane With Free Controls
Jones, Robert T. & Cohen, Doris
August 15, 1940
Primary view of Analysis of variation of piston temperature with piston dimensions and undercrown cooling
Sanders, J. C. & Schramm, W. B.
January 15, 1948
Primary view of An Analytic Study of Turbojet Engine Thrust Augmentation With Liquid Hydrogen, Pentaborane, Magnesium Slurry, and JP-4 Afterburner Fuels and a 220-Second Impulse Rocket
Morris, James F.
August 15, 1956
Primary view of Analytical investigation of single-stage-turbine efficiency characteristics in terms of work and speed requirements
Stewart, Warner L.
October 15, 1956
Primary view of Analytical Study of the Effect of Center-of-Gravity Position on the Response to Longitudinal Control in Landing Approaches of a Swept-Wing Airplane of Low Aspect Ratio Having No Horizontal Tail
Stone, Ralph W., Jr.
October 15, 1954
Primary view of Application of Theodorsen's propeller theory to the calculation of the performance of dual-rotating propellers
Gilman, Jean, Jr.
March 15, 1951
Primary view of Application of Theodorsen's theory to propeller design
Crigler, John L.
March 15, 1948
Primary view of Applications of power spectral analysis methods to maneuver loads obtained on jet fighter airplanes during service operations
Mayer, John P. & Hamer, Harold A.
January 15, 1957
Primary view of Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses
Heldenfels, Richard R. & Vosteen, Louis F.
May 15, 1957
Primary view of An assessment of the airplane drag problem at transonic and supersonic speeds
Donlan, Charles J.
July 15, 1954
Back to Top of Screen