Author: National Advisory Committee for Aeronautics / Publish Year Decade: 1950 - 1959 - Blacklight Search Results

Start Over Author National Advisory Committee for Aeronautics Publish Year Decade 1950 - 1959

501. Technical notes. 3994. Static strength of cross-grain 7075-16 aluminum-alloy extruded bar containing fatigue cracks [with list of references]; by Walter Dig and Arthur J. McEvily, jr.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1957
SuDoc number:: Y 3.N 21/5:6/(nos.)

502. Technical notes. 3997. Note on effect of beat transfer on peak pressure rise associated with separation of turbulent boundary layer on body of revolution (NACA RM-10) at Mach number of 1.61 [with list of references]; by K. R. Czarnecki and Archibald R. Sinclair.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1957
SuDoc number:: Y 3.N 21/5:6/(nos.)

503. Technical notes. 3998. Ground simulator studies of effects of valve friction, stick friction, flexibility, and backlash on power control system quality [with list of references]; by B. Porter-Brown.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1957
SuDoc number:: Y 3.N 21/5:6/(nos.)

504. Technical notes. 4010. Experimentally determined natural vibration modes of some cantileverwing flutter models by using acceleration method [with list of references]; by Perry W. Hanson and W. J. Tuovilla.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1957
SuDoc number:: Y 3.N 21/5:6/(nos.)

505. Reports (1956). 1276. Errata [Wind tunnel and flight investigations of use of leading-edge area suction for purpose of increasing maximum lift, coefficient of 35° sweptwing airplane] by Curt A. Holzhauser and Richard S. Bray.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 29, 1957
SuDoc number:: Y 3.N 21/5:5/(nos.)

506. Research memorandum RM (series). L57A11. Preliminary measurements of atmospheric turbulence at high altitude as determined from acceleration measurements on Lockheed U-2 airplane [with list of references]: by Thomas L. Coleman and Jack Funk.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 27, 1957
SuDoc number:: Y 3.N 21/5:15/(nos.)

507. Technical notes. 3230. Errata [Investigation of distributed surface roughness on body of revolution at Mach number of 1.61]. by K. R. Czarnecki, Ross B. Robinson, and John H. Hilton, Jr., June 1954.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [Mar. 22, 1957.]
SuDoc number:: Y 3.N 21/5:6/(nos.)

508. Research memorandum RM (series). E56K30. Survey of microstructures and mechanical properties of over-temperatured S-816 turbines buckets from J47 engines; by S. Floreen and R. A. Signorelli.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Washington, Mar. 20, 1957

509. Research memorandum RM (series). E57A29a. Evaluation of use of electrical resistance for detecting overtemperatured S-816 turbine blades [with list of references]; by Leonard Robins.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Mar. 20, 1957

510. Technical notes. 3941. Errata [Comparison of calculated and experimental load distributions on thin wings at high subsonic and sonic speeds], by John L. Crigler, Jan. 1957.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [Mar. 8, 1957.]
SuDoc number:: Y 3.N 21/5:6/(nos.)

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