UNT Libraries Government Documents Department - 19 Matching Results

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Primary view of Additional Studies of the Stability and Controllability of an Unswept-Wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques
Bates, William R.; Lovell, Powell M., Jr. & Smith, Charles C., Jr.
November 6, 1951
Primary view of Aerodynamic characteristics at transonic speeds of a 69 degree delta wing with a triangular plan-form control having a skewed hinge axis and an overhang balance: transonic-bump method
Wiley, Harleth G.
February 6, 1951
Primary view of Aerodynamic characteristics including pressure distribution of a fuselage and three combinations of the fuselage with swept-back wings at high subsonic speeds
Sutton, Fred B. & Martin, Andrew
February 6, 1951
Primary view of Aerodynamic Characteristics of Four Wings of Sweepback Angles 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees, NACA 65A006 Airfoil Section, Aspect Ratio 4, and Taper Ratio 0.6 in Combination With a Fuselage at High Subsonic Mach Numbers and at a Mach Number of 1.2
Luoma, Arvo A.
June 6, 1951
Primary view of Altitude-test-chamber investigation of performance of a 28-inch ram-jet engine 3: combustion and operational performance of three flame holders with a center pilot burner
Shillito, Thomas B.; Younger, George G. & Henzel, James G., Jr.
February 6, 1951
Primary view of Damping in a roll of a missile configuration with a modified triangular wing and a cruciform tail at a Mach number of 1.52
Scherrer, Richard & Dennis, David H.
March 6, 1951
Primary view of Effect of spark repetition rate on the ignition limits of a single tubular combustor
Foster, Hampton H.
December 6, 1951
Primary view of An Electromagnetic Flowmeter for Rocket Research
Jaffe, Leonard; Coss, Bert A. & Daykin, Donald R.
March 6, 1951
Primary view of Flight Instrument for Measurement of Liquid-Water Content in Clouds at Temperatures Above and Below Freezing
Perkins, Porter J.
March 6, 1951
Primary view of Investigation of Minimum Drag and Maximum Lift-Drag Ratios of Several Wing-Body Combinations Including a Cambered Triangular Wing at Low Reynolds Numbers and at Supersonic Speeds
Brown, Clinton E. & Hargrave, L. K.
August 6, 1951
Primary view of Matching Characteristics of J35-A-23 Compressor and Two-stage Turbine
Dugan, James F., Jr.; Rebeske, John J., Jr. & Finger, Harold B.
August 6, 1951
Primary view of Performance of single-stage compressor designed on basis of constant total enthalpy with symmetrical velocity diagram at all radii and velocity ratio of 0.7 at rotor hub
Burtt, Jack R. & Jackson, Robert J.
September 6, 1951
Primary view of Pressure Pulsations on Rigid Airfoils at Transonic Speeds
Humphreys, Milton D.
December 6, 1951
Primary view of Stability and control characteristics at low speed of a 1/5-scale model of the Edo 142 hydro-ski research airplane
Riebe, John M.; MacLeod, Richard G. & Moseley, William C., Jr.
August 6, 1951
Primary view of Static longitudinal stability and dynamic characteristics at high angles of attack and at low Reynolds numbers of a model of the X-3 supersonic research airplane
Burk, Sanger M., Jr. & Hultz, Burton E.
February 6, 1951
Primary view of Transonic-Wing Investigation in the Langley 8-Foot High-Speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2: Analysis of Pressure Distribution of Wing-Fuselage Configuration Having a Wing of 45 Degrees Sweptback, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section
Loving, Donald L. & Estabrooks, Bruce B.
September 6, 1951
Primary view of A transonic-wing investigation in the Langley 8-foot high-speed tunnel at high subsonic Mach numbers and at a Mach number of 1.2: Wing-fuselage configuration having a wing of 0 degrees sweepback, aspect ratio 4.0,taper ratio 0.6, and NACA 65A006 ai
Cahn, Maurice S. & Bryan, Carroll R.
March 6, 1951
Primary view of Wind-Tunnel Investigation at Low Speed of the Effects of Symmetrical Deflection of Half-Delta Tip Controls on the Damping in Roll and Yawing Moment Due to Rolling of a Triangular-Wing Model
Wolhart, Walter D.
April 6, 1951
Primary view of Wind-Tunnel Investigation at Subsonic and Low Transonic Speeds of the Effects of Aileron Span and Spanwise Location on the Rolling Characteristics of a Test Vehicle With Three Untapered 45 Degree Sweptback Wings
Johnson, Harold S.
April 6, 1951
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