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

Start Over Author National Advisory Committee for Aeronautics Sudoc Stem Y 3.N 21/5

6311. Flow. Effect of transition in cross-sectional shape on development of velocity and pressure distribution of turbulent flow in pipes [with list of references], by Edwin Mayer; [translation by S. Reiss from] VDI-Forschungsheft 389. supplement to Forschung auf dem gebiete des ingenieurwesens, edition B, v. 9, Mar.-Apr. 1938.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1939
SuDoc number:: Y 3.N 21/5:8/903

6312. Hulls (aircraft). Tanks tests to determine effects of chine flare of flying-boat bull, N. A. C. A. model series 62 and 69 [with list of references]; by Joe W. Bell and Roland E. Olson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1939
SuDoc number:: Y 3.N 21/5:6/725

6313. Ice. Adhesion of ice in its relation to de-icing of airplanes [with list of references]; by A. M. Rothrock and R. F. Selden.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1939
SuDoc number:: Y 3.N 21/5:6/723

6314. Impeller blades. Design of centrifugal impeller blades [with list of references], by A. Betz and I. Flügge-Lotz; [translation by S. Reiss from] Ingenieur-archiv, v. 9, Dec. 1938. Washington, July 1939.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [August 1939]
SuDoc number:: Y 3.N 21/5:8/902

6315. Stiffeners (aircraft). Stability of rectangular plates with longitudinal or transverse stiffeners under uniform compression [with list of references], by R. Barbré; [translation by W. L. Koch from] Ingenieur-archiv, v. 8. no. 2, 1937

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1939
SuDoc number:: Y 3.N 21/5:8/904

6316. Temperature-indicating paints [with list of references], by F. Penzig; [translation by S. Reiss from] Zeitschrift des Vereines Deutscher Ingenieure, v. 83, no. 3, Jan. 21, 1939.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1939
SuDoc number:: Y 3.N 21/5:8/905

6317. Wings. Effects of surface waviness and of rib stitching on wing drag [with list of references]; by Manley J. Hood.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Aug. 1939
SuDoc number:: Y 3.N 21/5:6/724

6318. Buckling (aircraft). Method of estimating critical buckling load for structural members [with list of references]; by Eugene E. Lundquist.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1939
SuDoc number:: Y 3.N 21/5:6/717

6319. Controls (aircraft). Effect of masses of controls on longitudinal stability with free elevator, by Rudolf Schmidt; [translation by S. Reiss from] Luftfahrtforschung, v. 16, no. 1, Jan. 10, 1939.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1939
SuDoc number:: Y 3.N 21/5:8/900

6320. Floats (aircraft). Hydrodynamic and aerodynamic tests of family of models of seaplane floats with varying angles of dead rise, N. A. C. A. models 57-A, 57-B, and 57-C [with list of references]; by John B. Parkinson, Roland E. Olson, and Rufus O. House.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1939
SuDoc number:: Y 3.N 21/5:6/716

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