1,624 Matching Results

Search Results

Results: 1 - 24 next
Primary view of Preservation of Documents by Lamination
Wilson, William K. & Forshee, B. W.
October 30, 1959
Primary view of Wing Pressure Distributions Over the Lift Range of the Convair XF-92A Delta-Wing Airplane at Subsonic and Transonic Speeds
Keener, Earl R. & Jordan, Gareth H.
November 30, 1955
Primary view of Investigation of Drag and Static Longitudinal and Lateral Stability Characteristics of a 1/15-Scale Model of the Grumman F11F-1F Airplane at Mach Numbers of 1.56, 1.76, 2.06, and 2.53
Turner, Kenneth L. & Fournier, Roger H.
November 30, 1956
Primary view of A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2
Phelps, E. Ray & Boyd, John W.
April 30, 1957
Primary view of Wind-Tunnel Investigation at High Subsonic Speeds of the Effects on Static Stability Characteristics of Various Modifications to a Swept-Wing Fighter-Type Airplane Model
Goodson, Kenneth W.
April 30, 1957
Primary view of Experimental Investigation at High Subsonic Speeds of the Rolling-Stability Derivatives of a 1/22 Scale Model of the Republic F-105 Airplane
Sleeman, William C., Jr. & Hayes, William C., Jr.
June 30, 1955
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Mach Numbers of 1.41, 1.61, and 2.01
Spearman, M. Leroy & Driver, Cornelius
September 30, 1955
Primary view of Investigation of the Static Stability Characteristics of Five Hypersonic Missile Configurations at Mach Numbers From 2.29 to 4.65
Turner, Kenneth L. & Appich, W. H., Jr.
June 30, 1958
Primary view of Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration With a Low-Aspect-Ratio Wing and Blunt Nose at Mach Numbers From 1.2 to 2.1
Brown, Clarence A., Jr.
September 30, 1957
Primary view of Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine: 1: Rotor Blades With 10 Tubes in Cooling-Air Passages
Ellerbrock, Herman H., Jr. & Stepka, Francis S.
July 30, 1950
Primary view of Preliminary Performance Data Obtained in a Full-Scale Free-Jet Investigation of a Side-Inlet Supersonic Diffuser
Farley, John M. & Smith, Ivan D.
November 30, 1954
Primary view of Analysis of Heat Transfer and Fluid Friction for Fully Developed Turbulent Flow of Supercritical Water With Variable Fluid Properties in a Smooth Tube
Deissler, R. G. & Taylor, M. F.
January 30, 1953
Primary view of Experimental and Theoretical Determination of Forces and Moments on a Store and on a Store- Pylon Combination Mounted on a 45 Degree Swept- Wing-Fuselage Configuration at a Mach Number of 1.61
Morris, Odell A.; Carlson, Harry W. & Geier, Douglas J.
January 30, 1958
Primary view of Performance of an Inlet Having a Variable-angle Two-dimensional Compression Surface and a Fixed-geometry Subsonic Diffuser for Application to Reduced Engine Rotative Speeds- Mach Numbers 0.66, 1.5, 1.7, and 2.0
Allen, John L.
January 30, 1958
Primary view of Low-Temperature Chemical Starting of a 200-Pound-Thrust JP-4 - Nitric Acid Rocket Engine Using a Three-Fluid Propellant Valve
Hennings, Glen & Morrell, Gerald
June 30, 1955
Primary view of Use of Highly Reactive Chemical Additives to Improve Afterburner Performance at Altitude
Wanhainen, John P. & Sivo, Joseph N.
September 30, 1958
Primary view of Tabulated Pressure Data for a Series of Controls on a 60 Degree Delta Wing at Mach Numbers of 1.61 and 2.01
Lord, Douglas R. & Czarnecki, K. R.
March 30, 1956
Primary view of Off-Design Performance of Divergent Ejectors
Beheim, Milton A.
September 30, 1958
Primary view of Performance of a Single Fuel-Vaporizing Combustor With Six Injectors Adapted for Gaseous Hydrogen
Wear, Jerrold D. & Smith, Arthur L.
November 30, 1955
Primary view of Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60
Robins, A. Warner
October 30, 1953
Primary view of Heat-transfer and operating characteristics of aluminum forced-convection and stainless-steel natural-convection water-cooled single-stage turbines
Freche, John C. & Diaguila, A. J.
June 30, 1950
Primary view of An analysis of the forces and pressure distribution on a wing with the leading edge swept back 37.25 degrees
Edwards, George G. & Boltz, Frederick W.
March 30, 1950
Primary view of A Design Study of Leading-Edge Inlets for Unswept Wings
Dannenberg, Robert E.
June 30, 1950
Primary view of Longitudinal characteristics of two 47.7 degree sweptback wings with aspect ratios of 5.1 and 6.0 at Reynolds numbers up to 10 x 10(exp 6)
Salmi, Reino J. & Carros, Robert J.
March 30, 1950
Back to Top of Screen