Author: National Aeronautics and Space Administration / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Sudoc Stem Y 3.N 21/5

751. NACA research memorandum RM (series). L56A03. Investigation of effects of body camber and body indentation on longitudinal characteristics of 60° deltawing-body combination at Mach number of 1,61 [with list of references]; by John R. Sevier, jr..

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

752. NACA research memorandum RM (series). L56A09. Effects upon body drag of jets exhausting from wing-mounted nacelles [with list of references]; by Robert W. Rainey.

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

753. NACA research memorandum RM (series). L56A25. Two experiments on applications of transonic area rule to asymmetric configurations [with list of references;] by James Rudyard Hall.

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

754. NACA research memorandum RM (series). E56A20a. Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation [with list of references]; by Allen J. Metzler and Jack S. Grobman.

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

755. NACA research memorandum RM (series). L56A16. Flight investigation of effect of propulsive jet positioned according to transonic area rule on drag coefficients of single-engine delta-wing configuration at Mach numbers from 0.83 to 1.36 [with list of references]; by Joseph H. Judd and Ralph A. Falanga.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 13, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

756. NACA research memorandum RM (series). L56B02. Transonic investigation of effectiveness and loading characteristics of flap-type Aileron with and without paddle balances on unswept-wingfuselage model [with list of references]; by Gerald Hieser.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 13, 1956
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

757. NACA research memorandum RM (series). E55K15. Effect of inlet-duct length in uniform-flow field on turbojet-engine operation [with list of references]; by Robert J. Lubick, Louis J. Chelko, and Lewis E. Wallner.

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

758. NACA research memorandum RM (series). E55J17a. Effect of combustion gas properties on turbojet-engine performance with hydrogen as fuel [with list of references]; by Robert E. English.

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

759. NACA research memorandum RM (series). E55K04. Effect of design compressor pressure ratio on performance of hypothetical 2-spool nuclear-powered turbojet engines [with list of references]; by James P. Dugan, jr.

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

760. NACA research memorandum RM (series). H55L28a. Flight Investigation of effect of vertical tail size on rolling behavior of swept-wing airplane having lateral-longitudinal coupling [with list of references]; by Thomas W. Finch, James R. Peele, Richard E. Day.

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

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