UNT Libraries Government Documents Department - 24 Matching Results

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Primary view of Boundary-Layer Transition at High Reynolds Numbers as Obtained in Flight of a 20 Degree Cone-Cylinder With Wall to Local Stream Temperature Ratios Near 1.0
Rabb, Leonard & Disher, John H.
November 3, 1955
Primary view of A Correlation of Two-Dimensional Data on Lift Coefficient Available With Blowing-, Suction-, Slotted-, and Plain-Flap High-Lift Devices
Riebe, John M.
October 3, 1955
Primary view of Drag and rolling-moment effectiveness of trailing-edge spoilers at Mach numbers 2.2 and 5.0
Canning, Thomas N. & DeRose, Charles E.
October 3, 1955
Primary view of Drag Near Zero Lift of a 1/7-Scale Model of the Convair B-58 External Store as Measured in Free Flight Between Mach Numbers of 0.8 and 2.45
Hopko, Russell N.
August 3, 1955
Primary view of Effect of surface-active additives on physical properties of slurries of vapor-process magnesium
Pinns, Murray L.
November 3, 1955
Primary view of Effects of Boundary-Layer Separation on Normal Force and Center of Pressure of a Cone-Cylinder Model With a Large Base Flare at Mach Numbers From 3.00 to 6.28
Dennis, David H. & Syvertson, Clarence A.
October 3, 1955
Primary view of Error in airspeed measurement due to the static-pressure field ahead of an airplane at transonic speeds
O'Bryan, Thomas C.; Danforth, Edward C. B. & Johnston, J. Ford
August 3, 1955
Primary view of Experimental Investigation of the Zero-Lift Wave Drag of Seven Pairs of Delta Wings With Constant and Varying Thickness Ratios at Mach Numbers of 1.62, 1.93, and 2.41
Henderson, Arthur, Jr.
June 3, 1955
Primary view of Exploratory Tests of Transpiration Cooling on a Porous 8 Degree Cone at M = 2.05 Using Nitrogen Gas, Helium Gas, and Water as the Coolants
Chauvin, Leo T. & Carter, Howard S.
June 3, 1955
Primary view of Grain Refinement Produced by an Alpha Phase Anneal of Beta Phase Heat Treated and Water Quenched Uranium
Gradner, H.R.
January 3, 1955
Primary view of Internal performance of a series of circular auxiliary-air inlets immersed in a turbulent boundary layer : Mach number range: 1.5 to 2.0
Simon, Paul C.
March 3, 1955
Primary view of Measured Effective Thermal Conductivity of Uranium Oxide Powder in Various Gases and Gas Mixtures
Boegli, J. S. & Deissler, R. G.
March 3, 1955
Primary view of Media for Air Cleaning and Air-Assay Purposes : Final Summary Report for Period Ending December 31, 1954
unknown creator
October 3, 1955
Primary view of A Method for Determining the Composition of Methanol-Trimethyl Borate Mixtures
Kaye, Samuel & Sordyl, Frank
November 3, 1955
Primary view of A method for the analysis of compounds containing boron, carbon, and hydrogen
Allen, Harrison, Jr. & Tannenbaum, Stanley
March 3, 1955
Primary view of NACA Conference on Engine Stall and Surge
unknown creator
February 3, 1955
Primary view of The Occlusion of Hydrogen by Uranium During Several Types of Beta Heat Treatments
Ray, William E.
March 3, 1955
Primary view of Performance of a double-cone inlet with and without a shroud at below-design Mach numbers
Pennington, Donald; Rabb, Leonard & Simpkinson, Scott H.
March 3, 1955
Primary view of Performance of as-forged, heat-treated, and overaged S-816 blades in a turbojet engine
Weeton, J. W.; Clauss, F. J. & Johnston, J. R.
March 3, 1955
Primary view of Performance of four experimental high btu-per-gallon fuels in a single turbojet combustor
Jonash, Edmund R.; Metzler, Allen J. & Butze, Helmut F.
November 3, 1955
Primary view of Temperature in a J47-25 Turbojet-Engine Combustor and Turbine Sections During Steady-State and Transient Operation in a Sea-Level Test Stand
Morse, C. R. & Johnston, J. R.
June 3, 1955
Primary view of Temperature Recovery Factors on a Slender 12 Degree Cone-Cylinder at Mach Numbers From 3.0 to 6.3 and Angles of Attack Up to 45 Degrees
Reller, John O. & Hamaker, Frank M.
October 3, 1955
Primary view of Wind-tunnel investigation at Mach 1.9 of multijet-missile base pressures
Baughman, L. Eugene
March 3, 1955
Primary view of Wind-Tunnel Measurements of the Dynamic Cross Derivative (Rolling Moment Due to Yawing Velocity and to Acceleration in Sideslip) of the Douglas D-558-II Airplane and Its Components at Supersonic Speeds Including Description of the Technique
Boatright, William B.
November 3, 1955
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