Author: National Aeronautics and Space Administration / Publisher: National Aeronautics and Space Administration - Blacklight Search Results

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16541. 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.)

16542. 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.)

16543. 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.)

16544. NACA research memorandum RM (series). A57A24. Wind-tunnel tests of static longitudinal characteristics at low speed of swept-wing airplane with slotted flaps, area-sunctlon flaps, and wing leading-edge devices [with list of references]; by Ralph L. Makl and Harry A. James.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 30, 1957
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

16545. NACA research memorandum RM (series). E56L19. Performance of external-compression bump inlet at Mach numbers of 1.5 to 2.0 [with one reference]; by Paul C. Simon, Dennis W. Brown, and Ronald G. Huff.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 24, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16546. NACA research memorandum RM (series). E57A31. Full-scale free-jet investigation of 2-shock side-inlet diffuser at Mach 2.75 and comparison with single-shock diffuser [with list of references]; by John E. McAulay.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 24, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16547. NACA research memorandum RM (series). E57B04. Experimental Investigation of performance of single-stage transonic compressor with guide vaaes turning counter to direction of rotor whirl [with list of references]: by Lawrence J. Jahnsen and Theodore E. Fessler.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 23, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16548. NACA research memorandum RM (series). A57B14. Flight investigation of area-suction and blowing boundary-layer control on trailing-edge flaps of 35° swept-wing carrier-type airplane [with list of references]; by Hervey C. Quigley, Francis W. K. Horn, and Robert C. Innls.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 22, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16549. NACA research memorandum RM (series). E55G01. Flight investigation of pentaborane fuel in 9.75-inch-diameter ramjet engine with downstream fuel injection [with list of references]; by John H. Disher and Merle L. Jones.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 22, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

16550. NACA research memorandum RM (series). L57B26. Investigation of static longitudinal stability characteristics at transonic speeds of 30° sweptback wing in wing-body configuration with and without horizontal tail [with list of references]; by Conrad M. Willis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 22, 1957
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

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