Publisher: National Aeronautics and Space Administration / Publish Year Decade: 1950 - 1959 - Blacklight Search Results

Start Over Publisher National Aeronautics and Space Administration Publish Year Decade 1950 - 1959

591. NACA research memorandum RM (series). E56H23. Performance of variable 2-dimensional inlet designed for engine-inlet matching: 1, Performance at design Mach number of 3.07 [with list of references]; by M. A. Beheim and L. W. Gertsma.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 20, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

592. NACA research memorandum RM (series). E56I18. Experimental investigation of high subsonic Mach number turbine having high rotor blade suction-surface diffusion [with list of references]; by William J. Nusbaum and Cavour H. Hauser.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 20, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

593. NACA research memorandum RM (series). L56H20. Investigation at supersonic speeds of effects of bomb-bay configuration upon aerodynamic characteristics of fuselages with non-circular cross sections [with list of references]; by Robert W. Rainey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 20, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

594. NACA research memorandum RM (series). E55H10. Performance of 4 experimental high-Btu-per-gallon fuels in single turbojet combustor [with list of references]; by Edmund R. Jonash. Allen J. Mettler, and Helmut F. Butxe.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 3, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

595. NACA research memorandum RM (series). A56H08. Large-scale wind-tunnel tests of airplane model with 45° sweptback wing of aspect ratio 2.8 with area suction applied to trailing-edge flaps and with several wing leading-edge modifications [with list of references]; by David G. Koenig and Kiyosi Aoyagi.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 2, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

596. NACA research memorandum RM (series). A56H31. Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers from 0.6 to 1.4 [with list of references]; by Earl D. Knechtel and Arvid N. Andrea.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 2, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

597. NACA research memorandum RM (series). L56H28a. Wind-tunnel investigation of development of lift on wings in accelerated longitudinal motion [with list of references]; by Thomas R. Turner.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 2, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

598. NACA research memorandum RM (series). A56G06. Experimental investigation at Mach numbers from 2.1 to 3.0 of Circular-internal-contraction inlets with translating centerbodies [with list of references]; by Emmet A. Mossman and Frank A. Pfyl.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

599. NACA research memorandum RM (series). L56H13. Static stability characteristics of cambered-delta-wing model at high subsonic speeds [with list of references]; by William C. Moseley, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

600. NACA research memorandum RM (series). L56H21. Effect of increase in angle of dead rise on hydrodynamic qualities of seaplane configuration incorporating high wing loading [with list of references]; by Walter J. Kapryan and Irving Woinstoin.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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