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Primary view of Acceleration Characteristics of a Turbojet Engine With Variable-Position Inlet Guide Vanes
Dobson, W. F. & Wallner, Lewis E.
July 7, 1955
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102B Airplane at Mach Numbers of 1.41, 1.61, and 2.01: Coord No. AF-231
Driver, Cornelius & Robinson, Ross B.
February 7, 1956
Primary view of Aerodynamic Characteristics of an 0.08-Scale Model of the Martin XB-51 Airplane at High Subsonic Speeds
Barnes, Robert H.
October 7, 1949
Primary view of The Aerodynamic Forces and Moments Exerted on a Spinning Model of the NY-1 Airplane as Measured by the Spinning Balance
Bamber, M. J. & Zimmerman, C. H.
February 7, 1933
Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Aerodynamic characteristics in sideslip of a large-scale model having a 63 degree swept-back vertical tail
McCormack, Gerald M.
October 7, 1949
Primary view of Aerodynamic Study of a Wing-Fuselage Combination Employing a Wing Swept Back 63 Degrees: Characteristics for Symmetrical Wing Sections at High Subsonic and Moderate Supersonic Mach Numbers
Mas, Newton A.
July 7, 1949
Primary view of Air flow around finned cylinders
Brevoort, M. J. & Rollin, Vern G.
November 7, 1935
Primary view of Analysis of coolant flow and pressure requirements for a return-flow turbine rotor blade design using hydrogen, helium, or air as coolant
Slone, Henry O. & Donoughe, Patrick L.
May 7, 1957
Primary view of Analysis of V-g data obtained from several naval airplanes
Thornton, James O.
July 7, 1950
Primary view of An Analysis of Vertical-Tail Loads Measured in Flight on a Swept-Wing Bomber Airplane
McGowan, William A. & Cooney, T. V.
May 7, 1957
Primary view of Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles
Hubbartt, James E. & Slone, Henry O.
September 7, 1955
Primary view of Average Skin-Friction Coefficients From Boundary-Layer Measurements in Flight on a Parabolic Body of Revolution (NACA RM-10) at Supersonic Speeds and at Large Reynolds Numbers
Rumsey, Charles B. & Loposer, J. Dan
March 7, 1951
Primary view of Bonded lead monoxide films as solid lubricants for temperatures up to 1250 degrees F
Sliney, Harold E. & Johnson, Robert L.
May 7, 1957
Primary view of Brief Studies of Turbojet Combustor and Fuel-System Operation With Hydrogen Fuel at -400 Degrees F
Straight, David M.; Smith, Arthur L. & Christenson, Harold H.
March 7, 1957
Primary view of The Calculation of the Path of a Jettisonable Nose Section
Goodwin, Roscoe H.
September 7, 1950
Primary view of Calibration of the Slotted Test Section of the Langley 8-Foot Transonic Tunnel and Preliminary Experimental Investigation of Boundary-Reflected Disturbances
Ritchie, Virgil S. & Pearson, Albin O.
July 7, 1952
Primary view of Combustion-efficiency and altitude-limit investigations of five fuels in an annular turbojet combustor
Wear, Jerrold D. & Jonash, Edmund R.
June 7, 1954
Primary view of Comparison of flight performance of AN-F-58 and AN-F-32 fuels in J35 turbojet engine
Acker, Loren W. & Kleinknecht, Kenneth S.
April 7, 1949
Primary view of Comparison of normal load factors experienced with jet fighter airplanes during combat operations with those of flight tests conducted by the NACA during operational training
Hamer, Harold A.; Huss, Carl R. & Mayer, John P.
July 7, 1954
Primary view of Comparison of the Aerodynamic Characteristics of the NACA 0010 and 0010-64 Airfoil Sections at High Subsonic Mach Numbers
Polentz, Perry P.
October 7, 1949
Primary view of Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings
Radin, Edward J. & Carpenter, Paul J.
October 7, 1953
Primary view of A comparison of the simulated-altitude performance of two turbojet combustor types
Bolz, Ray E.; Schroeter, Thomas T. & Zettle, Eugene V.
October 7, 1948
Primary view of Comparison of the Static Stability of a 68.7 Degree Delta-Wing Model with Dihedral and a Twisted and Cambered Wing Model of the Same Plan Form
Paulson, John W.
April 7, 1955
Primary view of Control Effectiveness Load and Hinge-Moment Characteristics of a Tip Control Surface on a Delta Wing at a Mach Number of 1.9
Conner, D. William & May, Ellery B., Jr.
October 7, 1949
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