Publish Year Decade: 1930 - 1939 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Publish Year Decade 1930 - 1939 Sudoc Stem Y 3.N 21/5

51. Load (mechanics). Load tests on stiffened circular cylindrical shell [with list of references], by E. Schnpitz and G. Krümling; [translation by S. Reiss from] Luftfahrtforschung, v. 14, no. 12, Dec. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1938
SuDoc number:: Y 3.N 21/5:8/864

52. Notches. Influence of notches under static stress [with list of references], by K. Matthaes; [translation by J. Vanier from] Luftfahrtforschung, v. 15, nos. 1 and 2, Jan. 20, 1938.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1938
SuDoc number:: Y 3.N 21/5:8/862

53. Seaplanes. On determination of take-off characteristics of seaplane [with list of references], by A. Perelmuter; [translation by S. Reiss from Report 255 of] Central Aero-Hydrodynamical Institute [Moscow, 1936].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1938
SuDoc number:: Y 3.N 21/5:8/863

54. Struts (aircraft). Compression struts with nonprogressively variable moment of inertia, by B. Rademski; [translation by J. Vanier from] Luftfahrtforschung, v. 14, no. 9, Sept. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1938
SuDoc number:: Y 3.N 21/5:8/861

55. Wings. Wind-tunnel tests of Clark Y wing having split flaps with gaps [with list of references]; by Carl J. Wenzinger.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1938
SuDoc number:: Y 3.N 21/5:6/650

56. Airplanes. Flight and wind-tunnel tests of XBM-1 dive bomber [with list of references]; by Philip Donely and Henry A. Pearson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1938
SuDoc number:: Y 3.N 21/5:6/644

57. Flight. Wind-tunnel tests of 2-engine airplane model as preliminary study of flight conditions arising on failure of one engine [with list of references]; by Edwin P. Hartman.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1938
SuDoc number:: Y 3.N 21/5:6/646

58. Floats (aircraft). Design of floats [with list of references], by W. Sottorf; [translation by J. A. Vanier from] Luftfahrtforschung, v. 14, nos. 4-5, Apr. 20, 1937.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1938
SuDoc number:: Y 3.N 21/5:8/860

59. Focke helicopter, by H. Focke; [translation by S. Reiss from] Luftwissen, v. 5, no. 2, Feb. 1938.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1938
SuDoc number:: Y 3.N 21/5:8/858

60. Fuel-oil. Engine performance and knock rating of fuels for high-output aircraft engines [with list of references]; by A. M. Rothrock and Arnold E. Biermann.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Apr. 1938
SuDoc number:: Y 3.N 21/5:6/647

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