UNT Libraries Government Documents Department - Browse

ABOUT BROWSE FEED
Primary view of Free-flight investigation of longitudinal stability and control of a rocket-propelled missile model having cruciform, triangular, inline wings and tails
Hall, James R
March 25, 1952
Primary view of Free-flight investigation of the control effectiveness of a differentially deflected horizontal tail at Mach numbers from 0.8 to 1.6
Mitchell, Jesse L & Vitale, A James
April 26, 1957
Primary view of Free-flight investigation of the drag of a model of a 60 degree delta-wing bomber with strut-mounted siamese nacelles and indented fuselage at Mach numbers from 0.80 to 1.35
Hoffman, Sherwood
September 25, 1957
Primary view of A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70
Falanga, Ralph A
March 8, 1956
Primary view of Free-flight investigation of the longitudinal stability and control of a rocket-propelled missile model having cruciform, triangular, interdigitated wings and tails
Sandahl, Carl A & Hall, James R
July 10, 1951
Primary view of Free-flight investigation of the rolling effectiveness at high subsonic, transonic, and supersonic speeds of leading-edge and trailing-edge ailerons in conjunction with tapered and untapered plan forms
Strass, H Kurt
July 23, 1948
Primary view of Free-flight investigation of the rolling effectiveness of a wing-spoiler arrangement at high subsonic, transonic, and supersonic speeds
Sandahl, Carl A
May 17, 1948
Primary view of An investigation of the aerodynamic characteristics at transonic Mach numbers of a swept-wing supersonic bomber configuration
Bielat, Ralph P & Cooper, J Lawrence
February 1, 1956
Primary view of Investigation of the aerodynamic characteristics of a model of a supersonic bomber configuration with a swept and an unswept wing at Mach numbers from 1.79 to 2.67
Silvers, H Norman & Zedekar, Raymond L
July 21, 1958
Primary view of An investigation of the aerodynamic characteristics of a series of cone-cylinder configurations at a Mach number of 6.86
Cooper, Ralph D & Robinson, Raymond A
December 17, 1951
Primary view of Investigation of Static Stability and Drag Characteristics of a 1/10-Scale Model of the Avco Booster Vehicle at Mach Numbers of 1.60 and 2.00, Coord. No. AF-AM-58
Church, James D. & Sista, Lawrence M.
May 10, 1957
Primary view of Effects of a J34 turbojet engine on supersonic diffuser performance
Beheim, Milton A & Englert, Gerald W
January 4, 1956
Primary view of Effects of a straightening operation on performance of Inconel 550 buckets
Gyorgak, C A; Johnston, J R & Weeton, J W
February 29, 1956
Primary view of Effects of additives on corrosion and mass transfer in sodium hydroxide - nickel systems under free-convection conditions
Forestieri, Americo F
August 2, 1954
Primary view of Effects of additives on pressure limits of flame propagation of propane-air mixtures
Belles, Frank E & Simon, Dorothy M
December 18, 1953
Primary view of Effects of altitude on turbojet engine performance
Fleming, William A
December 21, 1951
Primary view of Effects of compressor interstage bleed and adjustable inlet guide vanes on compressor stall characteristics of a high-pressure-ratio turbojet engine at altitude
Mallett, William E & Groesbeck, Donald E
January 17, 1956
Primary view of Effects of free-stream Reynolds number, engine installation, and model scale on stability characteristics of a translating-spike inlet at Mach 2.0
Musial, Norman T & Bowditch, David
November 13, 1957
Primary view of Effects of fuel temperature and fuel distribution on the combustion efficiency of a 16-inch ram-jet engine at a simulated Mach number of 2.9
Dangle, E E; Cervenka, A J & Bahr, D W
January 8, 1953
Primary view of Effects of inlet-flow-air distortion on steady-state altitude performance of an axial-flow turbojet engine
Conrad, E William; Hanson, Morgan P & Mcaulay, John E
September 27, 1955
Primary view of Effects of inlet icing on performance of axial-flow turbojet engine in natural icing conditions
Acker, Loren W & Kleinknecht, Kenneth S
May 25, 1950
Primary view of Effects of internal-area distribution, spike translation, and throat boundary-layer control on performance of a double-cone axisymmetric inlet at Mach numbers from 3.0 to 2.0
Conners, James F; Lovell, J Calvin & Wise, George A
August 30, 1957
Primary view of Effects of internal boundary-layer control on the performance of supersonic aft inlets
Obery, Leonard J & Schueller, Carl F
March 2, 1956
Primary view of Effect of ram-jet pressure pulsations on supersonic-diffuser performance
Connors, James F
November 20, 1950