UNT Libraries Government Documents Department - 158 Matching Results

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Primary view of Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 2: effect of compressor interstage air bleed
Rebeske, John J., Jr. & Dugan, James F., Jr.
July 3, 1953
Primary view of Aerodynamic characteristics at Mach number of 4.06 of a typical supersonic airplane model using body and vertical-tail wedges to improve directional stability
Dunning, Robert W.
December 3, 1957
Primary view of Aerodynamic characteristics at subsonic and supersonic Mach numbers of a thin triangular wing of aspect ratio 2 2: maximum thickness at midchord
Walker, Harold J. & Berggren, Robert E.
December 3, 1948
Primary view of The aerodynamic characteristics at transonic speeds of an all-movable, tapered, 45 degrees sweptback, aspect-ratio-4 tail surface deflected about a skewed hinge axis
Hammond, Alexander D. & Watson, James M.
July 3, 1952
Primary view of Aerodynamic Characteristics of a Model of an Escape Capsule for a Supersonic Bomber-Type Airplane at a Mach Number of 2.49
Presnell, John G., Jr.
December 3, 1957
Primary view of Altitude-Chamber Performance of British Roll-Royce Nene II Engine 4: Effect of Operational Variables on Temperature Distribution at Combustion-Chamber Outlets
Huntley, Sidney C.
July 3, 1950
Primary view of Altitude Investigation of Can-Type Flame Holder in 20-Inch-Diameter Ram-Jet Combustor
Smolak, George R. & Wentworth, Carl B.
June 3, 1954
Primary view of Altitude Investigation of Can-Type Flame Holder in 20-Inchdiameter Ram-Jet Combustor
Smolak, George R. & Wentworth, Carl B.
June 3, 1954
Primary view of Altitude Performance of J35-A-17 Turbojet Engine in an Altitude Chamber
Vincent, K. R. & Gale, B. M.
January 3, 1951
Primary view of Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine, Part 1, Performance and Windmilling Drag Characteristics
Fleming, William A.
August 3, 1948
Primary view of Altitude-wind-tunnel investigation of operational characteristics of J47 turbojet engine
Bloomer, Harry E.
August 3, 1950
Primary view of Aluminum borohydride as an ignition source for turbojet combustors
Straight, David M.; Fletcher, Edward A. & Foster, Hampton H.
September 3, 1953
Primary view of Analog computer study of some filtering, command-computer, and automatic-pilot problems connected with the attack phase of the automatically controlled supersonic interceptor
Sherman, Windsor L.
October 3, 1957
Primary view of Analysis of two-spool turboprop-engine characteristics
Davison, Elmer H.
June 3, 1957
Primary view of Analytical determination of effect of water injection on power output of turbine-propeller engine
Ross, Albert O. & Huppert, Merle C.
November 3, 1949
Primary view of Analytical investigation of flow through high-speed mixed-flow turbine
Stewart, Warner L.
October 3, 1951
Primary view of Approximate relative-total-pressure losses of an infinite cascade of supersonic blades with finite leading-edge thickness
Klapproth, John F.
March 3, 1950
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 Boundary-layer transition at supersonic speeds
Low, George M.
August 3, 1956
Primary view of Carbon deposition of 19 fuels in an annular turbojet combustor
Wear, Jerrold D. & Jonash, Edmund R.
February 3, 1949
Primary view of A comparison of the experimental and theoretical loading over triangular wings at supersonic speeds
Boyd, John W. & Phelps, E. Ray
January 3, 1951
Primary view of A Comparison of Two Techniques Utilizing Rocket-Propelled Vehicles for the Determination of the Damping-in-Roll Derivative
Stone, David G. & Sandahl, Carl A.
May 3, 1951
Primary view of Computed Performance of a Composite Engine Based on Experimental Data for a Single-Cylinder Conventional Aircraft Engine Converted to Compression-Ignition Operation
McCoy, J. Arnold & Szel, Frank
February 3, 1947
Primary view of Control characteristics of trailing-edge spoilers on untapered blunt trailing-edge wings of aspect ratio 2.7 with 0 degree and 45 degrees sweepback at Mach numbers of 1.41 and 1.96
Jacobsen, Carl R.
December 3, 1952
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