UNT Libraries Government Documents Department - 143 Matching Results

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Primary view of Aerodynamic characteristics at Mach number of 2.01 of two cruciform missile configurations having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with several canard controls
Spearman, M. Leroy & Robinson, Ross B.
August 30, 1954
Primary view of Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01
Spearman, M. Leroy
October 30, 1953
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Mach Numbers of 1.41, 1.61, and 2.01
Spearman, M. Leroy & Driver, Cornelius
September 30, 1955
Primary view of Aerodynamic characteristics of a two-blade NACA 10-(3)(12)-03 propeller
Allis, A. E. & Gray, W. H.
August 30, 1948
Primary view of The aerodynamic characteristics throughout the subsonic speed range of a thin, sharp-edged horizontal tail of aspect ratio 4 equipped with a constant-chord elevator
Bandettini, Angelo & Reed, Verlin D.
June 30, 1949
Primary view of Altitude performance evaluation of J71-A-11 turbojet engine
Useller, James W. & Pappas, George E.
March 30, 1956
Primary view of Analysis of a Form of Peak Holding Control
Delio, G. J.
March 30, 1956
Primary view of Analysis of Heat Transfer and Fluid Friction for Fully Developed Turbulent Flow of Supercritical Water With Variable Fluid Properties in a Smooth Tube
Deissler, R. G. & Taylor, M. F.
January 30, 1953
Primary view of An analysis of the forces and pressure distribution on a wing with the leading edge swept back 37.25 degrees
Edwards, George G. & Boltz, Frederick W.
March 30, 1950
Primary view of Analysis of two-stage-turbine efficiency characteristics in terms of work and speed requirements
Stewart, Warner L. & Wintucky, William T.
August 30, 1957
Primary view of Application of an ultraviolet spectrophotometric method to the estimation of alkylnaphthalenes in 10 experimental jet-propulsion fuels
Cleaves, Alden P. & Carver, Mildred S.
April 30, 1947
Primary view of Buffeting of External Fuel Tanks at High Speeds on a Grumman F7F-3 Airplane
Turner, Howard L.
January 30, 1947
Primary view of Calculated Aerodynamic Loadings of M, W, and Delta Wings in Incompressible Flow
Diederich, Franklin W. & Latham, W. Owen
August 30, 1951
Primary view of Calculated Lift Distributions of a Consolidated Vultee B-36 and Two Boeing B-47 Airplanes Coupled at the Wing Tips
Diederich, Franklin W. & Zlotnick, Martin
November 30, 1950
Primary view of Calculated Reactivity of Uranyl-Fluoride - Water Criticality Experiments
Bogart, Donald & Soffer, Leonard
March 30, 1956
Primary view of Characteristics of a canard-type missile configuration with an underslung scoop inlet at Mach numbers from 1.5 to 2.0
Fradenburgh, Evan A. & Campbell, Robert C.
January 30, 1953
Primary view of Characteristics of swept wings at high speeds
Donlan, Charles J. & Weil, Joseph
January 30, 1952
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 Comparison of theoretically and experimentally determined effects of oxide coatings supplied by fuel additives on uncooled turbine-blade temperature during transient turbojet-engine operation
Schafer, Louis J., Jr.; Stepka, Francis S. & Brown, W. Byron
March 30, 1953
Primary view of Component Performance Investigation of J71 Experimental Turbine 9 - Effect of First-Stator Adjustment;Internal Flow Conditions of J71-97 Turbine With 87-Percent-Design Stator Area
Schum, Harold J.; Petrash, Donald A. & Davison, Elmer H.
April 30, 1957
Primary view of Design and performance of an experimental axial-discharge mixed-flow compressor 3: over-all performance of impeller and supersonic-diffuser combination
Wilcox, Ward W. & Robbins, William H.
April 30, 1951
Primary view of Design considerations of a condensing system for vaporized magnesium
Witzke, Walter R.; Prok, George M. & Keller, Thomas A.
November 30, 1955
Primary view of A Design Study of Leading-Edge Inlets for Unswept Wings
Dannenberg, Robert E.
June 30, 1950
Primary view of Downwash survey behind two low-aspect-ratio variable-incidence wings in combination with three different size fuselages at a Mach number of 0.25
Hopkins, Edward J. & Sorensen, Norman E.
March 30, 1955
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