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Primary view of Thrust and Pumping Characteristics of a Series of Ejector-type Exhaust Nozzles at Subsonic and Supersonic Flight Speeds
Hearth, Donald P. & Valerino, Alfred S.
November 17, 1954
Primary view of Compatibility of Metals with Liquid Fluorine at High Pressures and Flow Velocities
Schmidt, Harold W.
April 17, 1958
Primary view of Transonic Aerodynamic and Trim Characteristics of a Multi-Engine Delta-Wing Airplane Model
Swihart, John M. & Foss, Willard E., Jr.
February 17, 1956
Primary view of Some Interference Effects That Influence Vertical-Tail Loads at Supersonic Speeds
Edwards, S. Sherman
February 17, 1956
Primary view of Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers From 0.6 to 18
Syvertson, Clarence A.; Gloria, Hermilo R. & Sarabia, Michael F.
September 17, 1958
Primary view of Evaluation of Some Aerodynamic Controls for a Low Aspect Ratio Missile
Winovich, Warren & Higdon, Nancy S.
July 17, 1958
Primary view of Method for Estimating Pitching-Moment Interference of Wing-Body Combinations at Supersonic Speed
Kaattari, George E.; Nielsen, Jack Norman & Pitts, William C.
April 17, 1952
Primary view of An Analog Study of the Influence of Internal Modifications to a Wing Leading Edge on Its Transient Temperature Rise During Highspeed Flight
Neel, Carr B.
March 17, 1958
Primary view of Aerodynamic Loads on an External Store Adjacent to an Unswept Wing at Mach Numbers Between 0.75 and 1.96
Hadaway, William M.
February 17, 1956
Primary view of Investigation of a 0.6 Hub-Tip Radius-Ratio Transonic Turbine Designed for Secondary-Flow Study 3 - Experimental Performance With Two Stator Configurations Designed to Eliminate Blade Wakes and Secondary-Flow Effects and Conclusions From Entire Stator Investigation
Rohlik, Harold E.; Wintucky, William T. & Moffitt, Thomas P.
September 17, 1957
Primary view of Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle
Rom, F. E. & Wachtl, W. W.
December 17, 1952
Primary view of Investigation of Ejection Releases of an MB-1 Rocket From a 0.04956-Scaled Model of the Convair F-106A Airplane at Several Mach Numbers and Simulated Altitudes
Lee, John B. & Basford, Robert C.
September 17, 1957
Primary view of Performance of a Supersonic Ramp-type Side Inlet With Ram-scoop Throat Bleed and Varying Fuselage Boundary-layer Removal Mach Number Range 1.5 to 2.0
Mitchell, Glenn A. & Campbell, Robert C.
January 17, 1957
Primary view of Influence of Automatic Control of Roll Coupling and Pitch-Up on Tail Loads
Stone, Ralph W., Jr.
June 17, 1957
Primary view of Total-Pressure Distortion and Recovery of Supersonic Nose Inlet With Conical Centerbody in Subsonic Icing Conditions
Gelder, Thomas F.
September 17, 1957
Primary view of Investigation of Wingless Missile Configurations with Folding Controls and Low-Aspect-Ratio Stabilizing Surfaces
Lazzeroni, Frank A.
September 17, 1958
Primary view of Aerodynamics of Oscillating Control Surfaces at Transonic Speeds
Thompson, Robert F. & Clevenson, Sherman A.
June 17, 1957
Primary view of Heat-Transfer Measurements on a Concave Hemispherical Nose Shape With Unsteady-Flow Effects at Mach Numbers of 1.98 and 4.95
Cooper, Morton; Beckwith, Ivan E.; Jones, Jim J. & Gallagher, James J.
July 17, 1958
Primary view of A Method for Predicting the Stability in Roll of Automatically Controlled Aircraft Based on the Experimental Determination of the Characteristics of an Automatic Pilot
Jones, Robert T. & Sternfield, Leonard
January 17, 1947
Primary view of Investigation of shock diffusers at Mach number 1.85 2: projecting double-shock cones
Moeckel, W. E.; Connors, J. F. & Schroeder, A. H.
June 17, 1947
Primary view of Analytical Investigation of Turbines With Adjustable Stator Blades and Effect of These Turbines on Jet-Engine Performance
Silvern, David H. & Slivka, William R.
July 17, 1950
Primary view of Low-Speed Aerodynamic Characteristics of a Series of Swept Wings Having NACA 65A006 Airfoil Sections (Revised)
Cahill, Jones F. & Gottlieb, Stanley M.
October 17, 1950
Primary view of The effect of tip tanks on the rolling characteristics at high subsonic Mach numbers of a wing having an aspect ratio of 3 with quarter-chord line swept back 35 degrees
Kuhn, Richard E. & Myers, Boyd C., II
January 17, 1950
Primary view of Preliminary Investigation of a Submerged Air Scoop Utilizing Boundary-Layer Suction to Obtain Increased Pressure Recovery
Nichols, Mark R. & Pierpont, P. Kenneth
March 17, 1950
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