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Primary view of An Aerodynamic Analysis of the Autogiro Rotor With a Comparison Between Calculated and Experimental Results
Wheatley, John B.
January 17, 1934
Primary view of Aerodynamic Heating and Boundary-Layer Transition on a 1/10-Power Nose Shape in Free Flight at Mach Numbers Up to 6.7 and Free-Stream Reynolds Numbers Up To 16 x 10(Exp 6)
Garland, Benjamine J.; Swanson, Andrew G. & Speegle, Katherine C.
June 17, 1957
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 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 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 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 Aerodynamic Performance of Several Techniques for Spike-Position Control of a Blunt-Lip Nose Inlet Having Internal Contraction; Mach Numbers of 0.63 and 1.5 to 2.0
Anderson, Arthur A. & Weinstein, Maynard I.
September 17, 1957
Primary view of Aerodynamics of Oscillating Control Surfaces at Transonic Speeds
Thompson, Robert F. & Clevenson, Sherman A.
June 17, 1957
Primary view of Airfoil profiles for minimum pressure drag at supersonic velocities: Application of shock-expansion theory, including consideration of hypersonic range
Chapman, Dean R.
September 17, 1952
Primary view of Altitude performance of pentaborane - JP-4 fuel blends in a modified J47 combustor
Branstetter, J. Robert & Kaufman, Warner B.
April 17, 1957
Primary view of Altitude-wind-tunnel investigation of several afterburner configurations having moderately high burner-inlet velocities
Schulze, F. W.; Bloomer, H. E. & Miller, R. R.
November 17, 1954
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 Analysis of a Nuclear-Powered Liquid-Metal Ducted-Fan Cycle
Rom, F. E. & Wachtl, W. W.
December 17, 1952
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 Analysis of experimental sea-level transient data and analog method of obtaining altitude response for turbine-propeller engine with relay-type speed control
Vasu, George & Pack, George J.
May 17, 1951
Primary view of An Analysis of Lateral Stability in Power-Off Flight With Charts for Use in Design
Zimmerman, Charles H.
November 17, 1936
Primary view of Analysis of Turbulent Heat Transfer, Mass Transfer, and Friction in Smooth Tubes at High Prandtl and Schmidt Numbers
Deissler, Robert G.
February 17, 1954
Primary view of Analytical Investigation of Ram-Jet-Engine Performance in Flight Mach Number Range From 3 to 7
Evans, Philip J., Jr.
October 17, 1951
Primary view of An Analytical Investigation of the Heat Losses from a U.S. Navy K-Type Airship
Hillendahl, Wesley H. & George, Ralph E.
February 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 An Analytical Study of the Comparative Performance of Four Air-Induction Systems for Turbojet-Powered Airplanes Designed to Operate at Mach Numbers Up to 1.5
Blackaby, James R.
June 17, 1952
Primary view of An Analytical Study of the Effects of Increasing Fin Chord on the Lift and Longitudinal Stability Characteristics of Constant-Span Fin-Body Combinations of Fineness Ratio 14
English, Roland D.
January 17, 1957
Primary view of Annual Report of the National Advisory Committee for Aeronautics (42nd): Administrative Report without Technical Reports
unknown creator
October 17, 1956
Primary view of Arrangement of Bodies of Revolution in Supersonic Flow to Reduce Wave Drag
Friedman, Morris D.
December 17, 1951
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