Author: National Advisory Committee for Aeronautics / Publisher: National Advisory Committee for Aeronautics / Publish Year Decade: 1940 - 1949 - Blacklight Search Results

Start Over Author National Advisory Committee for Aeronautics Publisher National Advisory Committee for Aeronautics Publish Year Decade 1940 - 1949

1. Technical memorandum. 1196. Nonstationary gas flow in thin pipes of variable cross section, by G. Guderly; translation [by Dave Feingold].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:8/(no.)

2. Technical notes. 1742. Stability and control characteristics at low speed of airplane model having 38.7° sweptback wing with aspect ratio 4.51. taper ratio 0.54. and Conventional tall surfaces [With list of references]; by Vernard E. Lockwood and James M. Watson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

3. Technical notes. 1762. Errata. Control considerations for optimum power proportionment in turbine-propeller engines; by Marcus F. Heidmann aad David Novik.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

4. Technical notes. 1772. Theoretical basic span loading characteristics of wings with arbitrary sweep, aspect ratio, and taper ratio [with list of references]; by Victor I. Stevens.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

5. Technical notes. 1773. Effects of variations in Reynolds number between 3.0x104and 25.0X104upon aerodynamic characteristics of number of NACA 6-series airfoil sections [with list of references]; by Laurence K. Loftin, jr., and William J. Bursnall.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

6. Technical notes. 1774. Calculated performance of compression-ignition engine-compressor-turbine combination based on experimental data [with list of references]; by Alexander Mendelson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

7. Technical notes. 1776. Hydrodynamic impact loads in rough water for prismatic float having angle of dead rise of 30° [with list of references]; by Robert W. Miller.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

8. Technical notes. 1779. Effects of antispin fillets and dorsal fins on spin and recovery characteristics of airplanes as determined from free-spinning-tunnel tests [with list of references]; by Lawrence J. Gale and Ira P. Jones, jr.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

9. Technical notes. 1780. Charts for conical part of downwash field of swept wings at supersonic speeds [with list of references]; by Jack N. Nielsen and Edward W. Perkins.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

10. Technical notes. 1783. Analysis of airspeeds and normal accelerations of Boeing B-247 and B-247D airplanes in commercial transport operation [with list of references]; by Walter G. Walker and Ivan K. Hadlock.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: Dec. 1948
SuDoc number:: Y 3.N 21/5:6/(nos.)

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