Author: National Advisory Committee for Aeronautics / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

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6561. Altimeters. Sonic altimeter for aircraft [with list of references]; by C. S. Draper.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:6/611

6562. Cylinders. Behavior of thin-wall monocoque cylinders under torsional vibration; by Robert E. Pekelsma.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:6/607

6563. Engines. Effect of air-entry angle on performance of 2-stroke-cycle compressionignition engine [with list of references]; by Sherod L. Earle and Francis J. Dutee.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:6/610

6564. Propellers. Ground effect on lifting propellers [with one reference], by A. Betz; [translation by S. Reiss from] Zeitschrift für angewandte mathematik und mechanik, v. 17, no. 2, Apr. 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:8/836

6565. Spin (aircraft). Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails: 1, Basic loading condition [with list of references]: by Oscar Seidman and A. I. Neihouse.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:6/608

6566. Wings. Empirical corrections to span load distribution at tip [with list of references]; by H. A. Pearson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:6/606

6567. Wings. Pressure distribution on wing section with slotted flap in free flight tests [with one reference], by Georg Kiel: [translation by J. Vanier from] Luftfahrtforschung, v. 14, no. 2, Feb. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:8/835

6568. Airplanes. Full-scale wind-tunnel and flight tests of Fairchild 22 airplane equipped with external-airfoil flaps [with list of references]; by Warren D. Reed and William C. Clay.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:6/604

6569. Cylinders. Stability of orthotopic elliptic cylinders in pure bending [with list of references], by O. S. Heck; [translation by J. Vanier from] Luftfahrtforschung, v. 14, no. 3, Mar. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:8/834

6570. Plates (metal). Apparent width of plate in compression [with list of references], by Karl Margnerre; [translation by J. Vanier from] Luftfahrtforschung, v. 14, no. 3, Mar. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1937
SuDoc number:: Y 3.N 21/5:8/833

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