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

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

771. NACA research memorandum RM (series). E55J18a. Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades [with list of references]; by Arthur N. Curren and Charles F. Zalabak.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 24, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

772. NACA research memorandum RM (series). E55G27. Effects of compressor interstage bleed and adjustable inlet guide vanes on compressor stall characteristics of high-pressure-ratio turbojet engine at altitude [with list of references]; by William E. Mallett and Donald E. Groesbeek.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 17, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

773. NACA research memorandum RM (series). E55J18. Comparison of performance and component frontal areas of hypothetical 2-spool and 1-spool turbojet engines; [with list of references]; by James F. Dngan, Jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 17, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

774. NACA research memorandum RM (series). L55I20. Effect of large negative dihedral of horizontal tail on longitudinal and lateral stability characteristics of swept-wing configuration at transonic speeds [with list of references]; by Donald D. Arabian.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 17, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

775. NACA research memorandum RM (series). L55I29. Low-speed pressure-distribution investigation of spoiler and spoilerslot-deflector on 30° sweptback wing-fuselage model having aspect ratio of 3, taper ratio of 0.5, and NACA 65A004 airfoil section [with list of references]; by Alexander D. Hammond.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 11, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

776. NACA research memorandum RM (series). L55H22a. Flight determination of drag and pressure recovery of 2 scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8 [with list of references]; by Leonard W. Putland.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 10, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

777. NACA research memorandum RM (series). L55I19. Wind-tunnel investigation of damping in roll of Bell X-1A research airplane and its components at supersonic speeds [with list of ref. erences]; by Russell W. McDearmon and Frank L. Clark.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 10, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

778. NACA research memorandum RM (series). L55J07. Transonic investigation of changing indentation design Mach number on aerodynamic characteristics of 45° sweptback-wing-body combination designed for high performance [with list of references]; by Donald L. Loving.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 10, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

779. NACA research memorandum RM (series). L57J07a. Investigation of tantalum In 3,800° F supersonic airstream [with list of references]; by Otto F. Trout, jr., and Jerry L. Modisette.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 9, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

780. NACA research memorandum RM (series). E55I21. Effects of J34 turbojet engine on supersonic diffuser performance [with list of references]; by Milton A. Behelm and Gerald W. Bnglert.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 4, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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