Publish Year Decade: 1950 - 1959 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Sudoc Stem Y 3.N 21/5

3361. NACA research memorandum RM (series). E52E13. Influence of canard-type control surface on flow field in vicinity of symmetrical fuselage at Mach numbers 1.8 and 2.0 [with list of references]; by George A. Wise and Murray Drver.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 16, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

3362. NACA research memorandum RM (series). E52E20. Survey of some preliminary investigations of supersonic diffusers at high Mach numbers [with list of references]: by Edgar M. Cortright, jr., and James F. Connors.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 10, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

3363. NACA research memorandum RM (series). E52B29. Over-all performance of J71 3-stage turbine [with one reference]; by William E. Berkey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 9, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

3364. Technical memorandums. 1346. Nonlinear theory of hot-wire anemometer [with list of references]; by R. Betchov; translation [by Mary L. Mahler].

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1952
SuDoc number:: Y 3.N 21/5:8/(nos.)

3365. Technical notes. 2489. Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes [with list of references]; by John M. Riebe and Rodger L. Naeseth. Washington, June 1952.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [July 1952]
SuDoc number:: Y 3.N 21/5:6/(nos.)

3366. Technical notes. 2643. Span load distributions resulting from angle of attack, rolling, and pitching for tapered swept back wings with streamwise tips, supersonic leading and trailing edges [with list of references]; by John C. Martin and Isabella Jeffreys.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1952
SuDoc number:: Y 3.N 21/5:6/(nos.)

3367. Technical notes. 2675. Measurements of flying qualities of F-47D-30 airplane to determine lateral and directional stability and control characteristics [with list of references]; by R. Fabian Goranson and Christopher C. Kraft, jr.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: July 1952
SuDoc number:: Y 3.N 21/5:6/(nos.)

3368. Technical notes. 2689. Effect of high-lift devices on low-speed static lateral and yawing stability characteristics of untapered 45° sweptback wing [with list of references]; by Jacob H. Lichtenstein. Washington, May 1952.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [July 1952]
SuDoc number:: Y 3.N 21/5:6/(nos.)

3369. Technical notes. 2695. Migration of cobalt during firing of ground-coat enamels on iron [with list of references]: by William N. Harrison, Joseph C. Richmond, Joseph W. Pitts, and Stanley G. Benner. Washington, June 1952.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [July 1952]
SuDoc number:: Y 3.N 21/5:6/(nos.)

3370. Technical notes. 2697. Method and graphs for evaluation of air-induction systems [with list of references]; by George B. Brajnikoff. Washington, May 1952.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [July 1952]
SuDoc number:: Y 3.N 21/5:6/(nos.)

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