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Primary view of Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 3: effect of turbine stator adjustment
Rohlik, Harold E. & Rebeske, John J.
August 2, 1954
Primary view of Adaptation of Combustion Principles to Aircraft Propulsion Volume 2: Combustion in Air-Breathing Jet Engines
Fuels and Combustion Research Division
May 2, 1956
Primary view of Aerodynamic characteristics at Mach numbers from 0.7 to 1.75 of a four-engine swept-wing airplane configuration as obtained from a rocket-propelled model test
Chapman, Rowe, Jr.
September 2, 1955
Primary view of Aerodynamic characteristics of a 68.4 degree delta wing at Mach numbers of 1.6 and 1.9 over a wide Reynolds number range
Hatch, John E., Jr. & Gallagher, James J.
November 2, 1953
Primary view of The aerodynamic characteristics of a body in the two-dimensional flow field of a circular-arc wing at a Mach number of 2.01
Gapcynski, John P. & Carlson, Harry W.
July 2, 1957
Primary view of Aerodynamic characteristics of a two-blade NACA 10-(3)(08)-03R propeller
Evans, Albert J. & Salters, Leland B., Jr.
September 2, 1948
Primary view of Aerodynamic Characteristics of Low-aspect-ratio Wings at High Supersonic Mach Numbers
Ulmann, Edward F. & Bertram, Mitchel H.
November 2, 1953
Primary view of Aerodynamic characteristics of low-aspect-ratio wings at high supersonic Mach numbers
Ulmann, Edward F. & Bertram, Mitchel H.
November 2, 1953
Primary view of Aerodynamic characteristics of two flat-bottomed bodies at Mach number of 3.12
Jack, John R. & Moskowitz, Barry
April 2, 1954
Primary view of Aerodynamic characteristics of two-plane, unswept tapered wings of aspect ratio 3 and 3-percent thickness from tests on a transonic bump
Emerson, Horace F. & Gale, Bernard M.
May 2, 1952
Primary view of Aerodynamic characteristics with fixed and free transition of a modified delta wing in combination with fuselage at high subsonic speeds
Polhamus, Edward C. & King, Thomas J., Jr.
May 2, 1950
Primary view of Altitude Operation of Gas-Turbine Engine With Variable-Area Fuel-Nozzle System
Gold, H. & Rosenzweig, S.
April 2, 1951
Primary view of Altitude-Test-Chamber Investigation of McDonnell Afterburner on J34 Engine
Reller, John O. & Dowman, Harry W.
June 2, 1949
Primary view of Altitude-wind-tunnel investigation of AN-F-58 fuel in experimental version of J47 turbojet engine
Meyer, Carl L.
May 2, 1949
Primary view of Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings 5 - Curtiss 836-14C2-18R1 Four-Blade Propeller
Saari, Martin J. & Wallner, Lewis E.
December 2, 1946
Primary view of Analysis of effects of airplane characteristics and autopilot parameters on a roll-command system with aileron rate and deflection limiting
Schy, Albert A. & Gates, Ordway B., Jr.
September 2, 1955
Primary view of Analysis of Performance of Jet Engine From Characteristics of Components 2: Interaction of Components as Determined From Engine Operation
Goldstein, Arthur W.; Alpert, Sumner; Beede, William & Kovach, Karl
June 2, 1948
Primary view of Analysis of several methods of pumping cooling air for turbojet engine afterburners
Samuels, John C. & Yanowitz, Herbert
February 2, 1953
Primary view of Analysis of turbomachine viscous losses affected by changes in blade geometry
Miser, James W.; Stewart, Warner L. & Whitney, Warren J.
October 2, 1956
Primary view of An Application of the Rocket-Propelled-Model Technique to the Investigation of Low-Lift Buffeting and the Results of Preliminary Tests
Mason, Homer P. & Gardner, William N.
September 2, 1952
Primary view of An Approximate Method for Estimating the Incompressible Laminar Boundary-Layer Characteristics on a Flat Plate in Slipping Flow
Donaldson, Coleman duP.
May 2, 1949
Primary view of Characteristics of a 15-Percent-Chord and a 35-Percent-Chord Plain Flap on the NACA 0006 Airfoil Section at High Subsonic Speeds
Ilk, Richard J.
October 2, 1947
Primary view of Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7
Brun, Rinaldo J.
November 2, 1955
Primary view of Collection and summary of flap-type-aileron rolling-effectiveness data at zero lift as determined by rocket-powered model tests at Mach numbers between 0.6 and 1.6
Strass, H. Kurt; Stephens, Emily W.; Fields, E. M. & Schult, Eugene D.
September 2, 1955
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