UNT Libraries Government Documents Department - 173 Matching Results

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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 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 Lateral Stability and Control Measurements of a Fighter-Type Airplane With a Low-Aspect-Ratio Unswept Wing and a Tee-Tail
Arabian, Donald D. & Schmeer, James W.
June 12, 1956
Primary view of Cascade Investigation of Cooling Characteristics of a Castfinned Air-Cooled Turbine Blade for Use in a Turboprop Engine
Stepka, Francis S.; Richards, Hadley T. & Hickel, Robert O.
June 12, 1957
Primary view of Summary of Subsonic-Diffuser Data
Henry, John R.; Wood, Charles C. & Wilbur, Stafford W.
October 12, 1956
Primary view of Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-Aspect-Ratio Swept-Back Wing-Stability and Control
Smith, Willard G.
January 12, 1953
Primary view of Free-flight Tests of 45 Deg Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds
O'Kelly, Burke R.; Lundstrom, Reginald R. & Lauten, William T., Jr.
October 12, 1954
Primary view of Aerodynamic loadings associated with swept and unswept spoilers on a flat-plate at Mach numbers of 1.61 and 2.01
Lord, Douglas R. & Czarnecki, K. R.
March 12, 1956
Primary view of Natural Icing of an Axial-Flow Turbojet Engine in Flight for a Single Icing Condition
Acker, Loren W.
August 12, 1948
Primary view of Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine. 7: Rotor-Blade Fabrication Procedures
Long, Roger A. & Esgar, Jack B.
September 12, 1951
Primary view of A Method for Calculating the Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds
Nielsen, Jack Norman; Kaattari, George E. & Anastasio, Robert F.
November 12, 1953
Primary view of Rocket-Powered-Model Investigation of the Effects of Aeroelasticity on the Rolling Effectiveness of an 8.06-Percent-Scale McDonnell F3H-1 Airplane Wing at Mach Numbers From 0.5 to 1.4
English, Roland D.
April 12, 1954
Primary view of A Review of NACA Research Through 1954 on Boron Compounds as Fuels for Jet Aircraft (Project Zip)
Olson, Walter T.; Breitwieser, Roland & Gibbons, Louis C.
April 12, 1957
Primary view of Local Heat Transfer to Blunt Noses at High Supersonic Speeds
Stoney, William E., Jr.
July 12, 1957
Primary view of Effect of Several Jet-Engine Air-Inlet Configurations on the Low-Speed Static Longitudinal Stability Characteristics and Quantity Flow of a 1/6-Scale Model of the MX-1764 Airplane
Croom, Delwin R.
January 12, 1954
Primary view of High Mach Number, Low-Cowl-Drag, External-Compression Inlet With Subsonic Dump Diffuser
Connors, James F. & Flaherty, Richard J.
May 12, 1958
Primary view of An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
Gerus, Theodore F.; Powers, Albert G. & Heppler, Herbert J.
May 12, 1958
Primary view of Some Factors Affecting the Static Longitudinal and Directional Stability Characteristics of Supersonic Aircraft Configurations
Spearman, M. Leroy
July 12, 1957
Primary view of In-Flight Gains Realized by Modifying a Twin Side-Inlet Induction System
Saltzman, Edwin J.
December 12, 1957
Primary view of Total-Pressure-Recovery Characteristics of a Model of the McDonnell XF3H-1 Inlets and Forebody in a Free Jet at a Mach Number of 1.55
Merlet, Charles F. & Carter, Howard S.
March 12, 1952
Primary view of Effects of Some Configuration Changes on Afterburner Combustion Performance
Nakanishi, Shigeo & King, Charles R.
June 12, 1957
Primary view of Preliminary Investigation of a Ceramic Lining for a Combustion Chamber for Gas-Turbine Use
Woodward, William H. & Bobrowsky, A. R.
April 12, 1948
Primary view of Preliminary investigation of spoiler lateral control on a 42 degree sweptback wing at transonic speeds
Schneiter, Leslie E. & Ziff, Howard L.
August 12, 1947
Primary view of Full-Scale Investigation of the Maximum Lift and Flow Characteristics of an Airplane Having Approximately Triangular Plan Form
Wilson, Herbert A., Jr. & Lovell, J. Calvin
February 12, 1947
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