Author: National Advisory Committee for Aeronautics / Publish Year Decade: 1930 - 1939 - Blacklight Search Results

Start Over Author National Advisory Committee for Aeronautics Publish Year Decade 1930 - 1939

151. Boundary layers. Effect of curvature on transition from laminar to turbulent boundary layer [with list of references]; by Milton Clauser and Francis Clauser.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1937
SuDoc number:: Y 3.N 21/5:6/613

152. Fuselage. Fuselage-drag tests in variable-density wind tunnel: Streamline bodies of revolution, fineness ratio of 5 [with list of references]: by Ira H Abbott.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1937
SuDoc number:: Y 3.N 21/5:6/614

153. Fuselage. Strength of shell bodies, theory and practice [with list of references], by H. Ebner; [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:: Sept. 1937
SuDoc number:: Y 3.N 21/5:8/838

154. Trusses (aircraft). Charts for checking stability of plane systems of rods [with list of references], by K. Borkmann; [translation by S. Reiss from] Luftfahrtforschung, v. 14, no. 2, Feb. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1937
SuDoc number:: Y 3.N 21/5:8/837

155. Wings. Spinning characteristics of wings: 3, Rectangular and tapered Clark Y monoplane wing with rovincled tips [with list or referencesi; by M. J. Bamber and R. O. House.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Sept. 1937
SuDoc number:: Y 3.N 21/5:6/612

156. Ailerons. Considerations affecting additional weight required in mass balance of ailerons [with list of references]; by W. S. Diehl.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1937
SuDoc number:: Y 3.N 21/5:6/609

157. 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

158. 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

159. 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

160. 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

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