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

501. NACA research memorandum RM (series). E57C06. Investigation of translating-double-cone axisymmetric inlets with cowl projected areas 40 and 20 percent of maximum at Mach numbers from 3.0 to 2.0 [with list of references]; by James F. Connors, George A. Wise, and J. Calvin Lovell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 20, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

502. NACA research memorandum RM (series). E57C12. Origin and development of leading-edge cracks in turbojet engine buckets [with list of references]; by D. F. Springsteen, C. A. Gyorgak, and J. R. Johnston.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 20, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

503. NACA research memorandum RM (series). A57A02. Investigation of wing-body juncture interference effects at transonic speeds for several swept-wing and body combinations [with list of references]; by John B. McDevitt and Robert A. Taylor.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 16, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

504. NACA research memorandum RM (series). L57B27. Flight investigation to determine effectiveness of Mach number 1.0, 1.2, and 1.41 fuselage indentations for reducing pressure drag of 45° sweptback wing configuration at transonic and low supersonic speeds [with list of references]; by Willard S. Blanchard, jr., and Sherwood Hoffman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 16, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

505. NACA research memorandum RM (series). L57C15. Wind-tunnel investigation of low-amplitude damping in yaw and directional stability of fuselage-tail configuration at Mach numbers up to 1.10 [with list of references]; by William E. Palmer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 16, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

506. NACA research memorandum RM (series). L57D18c. Preliminary results from free-flight investigation of boundary-layer transition and heat transfer on highly polished 8-inch diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds, numbers based on length of 1 foot up to 17.7 x 10 8 [with list of references]; by James R. Hall, Katherine C. Speegle, and Robert O. Piland.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 16, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

507. NACA research memorandum KM (series). A57C19. Airborne-target simulator for use with scope-presentation type firecontrol systems [with list of references]; by John V. Foster, Elmer C. Fulcher, and Donovan B. Heinle.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 10, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

508. NACA research memorandum RM (series). L57C13. Free-flight investigation to determine some effects of tall damping and wing-tail interference on rolling effectiveness of ailerons and spoiler on modified-delta wing at Mach numbers from 0.6 to 1.5 [with list of references]; by Roland D. English.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 10, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

509. NACA research memorandum RM (series). L57C21. Free-flight performance of rotating-vane-spoiler roll control system with low actuating forces [with list of references]; by Eugene D. Schult.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 10, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

510. NACA research memorandum RM (series). E57B18. Analysis of coolant flow and pressure requirements for return-flow turbine rotor blade design using hydrogen, helium, or air as coolant [with list of references]; by Henry O. Slone and Patrick L. Donoughe.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 7, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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