UNT Libraries Government Documents Department - 5,157 Matching Results

Search Results

Primary view of Investigations toward simplification of missile control systems
Curfman, Howard J., Jr.; Strass, H. Kurt & Crane, Harold L.
November 12, 1953
Primary view of Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings
Radin, Edward J. & Carpenter, Paul J.
October 7, 1953
Primary view of Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data
Burrows, Dale L.
June 17, 1954
Primary view of Wind-Tunnel Investigation to Determine the Horizontal- and Vertical-Tail Contributions to the Static Lateral Stability Characteristics of a Complete-Model Swept-Wing Configuration at High Subsonic Speeds
Wiggins, James W.; Kuhn, Richard E. & Fournier, Paul G.
July 10, 1953
Primary view of Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26
Martz, C. William & Goslee, John W.
October 30, 1953
Primary view of A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36 degrees
Cooper, Morton; Gapcynski, John P. & Hasel, Lowell E.
October 30, 1952
Primary view of A study of the use of various high-lift devices on the horizontal tail of a canard airplane model as a means of increasing the allowable center-of-gravity travel
Johnson, Joseph L., Jr.
January 21, 1953
Primary view of The Effects of a Small Jet of Air Exhausting From the Nose of a Body of Revolution in Supersonic Flow
Love, Eugene S.
November 12, 1952
Primary view of Investigation of the Aerodynamic Characteristics of the NACA RM-10 Missile (With Fins) at a Mach Number of 1.62 in the Langley 9-Inch Supersonic Tunnel
Coletti, Donald E.
December 19, 1952
Primary view of An experimental study of five annular air inlet configurations at subsonic and transonic speeds
Pendley, Robert E.; Milillo, Joseph R.; Fleming, Frank F. & Bryan, Carroll R.
August 19, 1953
Primary view of Transonic Wind-Tunnel Tests of the Launch, Jettison, and Longitudinal Characteristics of an Airplane and Missile Model Combination
Cleary, Joseph W.; Frank, Joseph L. & Dewey, C. Forbes, Jr.
November 20, 1957
Primary view of Theoretical Analysis of the Interference Effects of Several Supersonic Tunnel Walls Capable of Absorbing the Shock Caused by the Nose of a Model
Matthews, Clarence W.
May 26, 1958
Primary view of Some Effects of Aileron Deflection on the Static Lateral and Directional Aerodynamic Characteristics of Four Contemporary Airplane Models
Smith, Willard G. & Intrieri, Peter F.
July 23, 1957
Primary view of Preliminary Analysis of a Nuclear Powered Supersonic Airplane Using Ramjet Engines
Weber, Richard J. & Connolley, Donald J.
April 11, 1958
Primary view of Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Turbine Failure Investigation of J65-W-4 Turbojet Engine in an Altitude Test Chamber
McAulay, John E.; Braithwaite, Willis M. & Ciepluch, Carl C.
September 21, 1956
Primary view of Free Flight Investigation at Transonic Speeds of the Power-on Characteristics Including Some Effects of Sonic Propulsive Jets of a Four Engine Delta Wing Configuration
Falanga, Ralph A. & Judd, Joseph H.
August 16, 1957
Primary view of Hydrodynamic Characteristics of Missiles Launched Under Water
Dawson, John R.
June 27, 1958
Primary view of A Preliminary Investigation of the Performance of a Short Length Turbojet Combustor Using Vaporized Hydrocarbon Fuels
Jones, R. E. & Pawlik, E. V.
January 7, 1958
Primary view of Heat-Exchanger-Core Weights for Use With Hydrogen-Expansion Turbine
Reynolds, Thaine W.
October 3, 1957
Primary view of Altitude chamber evaluation of an aircraft liquid hydrogen fuel system used with a turbojet engine
Braithwaite, Willis M.; Fenn, David B. & Algranti, Joseph S.
August 19, 1957
Primary view of Hydrogen for Turbojet and Ramjet Powered Flight
Lewis Flight Propulsion Laboratory
April 26, 1957
Primary view of High Altitude Performance Investigation of J65-B-3 Turbojet Engine With Both JP-4 and Gaseous Hydrogen Fuels
Kaufman, Harold R.
April 2, 1957
Primary view of Analysis of turbojet and ram-jet engine cycles using various fuels
Wilcox, E. Clinton; Weber, Richard J. & Tower, Leonard K.
November 27, 1956
Back to Top of Screen