Catalog Issue Year Decade: 1960 - 1969 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Catalog Issue Year Decade 1960 - 1969 Sudoc Stem Y 3.N 21/5

381. NACA research memorandum RM (series). L55L26. Longitudinal characteristics of unswept-wing fighter-type model with external stores at Mach number of 1.82 and some effects of horizontal-tail and yaw-damper-vane deflection on sideslip derivatives [with list of references]; by Rosa B. Robinson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 23, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

382. NACA research memorandum RM (series). E56E04. Investigation of turbines suitable for use in turbojet engine with high compressor pressure ratio and low compressor-tip speed: 6, Experimental performance of 2-stage turbine [with list of references]; by Elmer H. Davison, Harold J. Schum, and Donald A. Petrash.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 20, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

383. NACA research memorandum RM (series). E55K16. Weight-flow and thrust limitations due to use of rotating combustors in turbojet engine [with list of references]; by Erwin A. Lezberg, Perry L. Blackshear, jr. and Warren D. Rayle.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 17, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

384. NACA research memorandum RM (series). E56D27. Performance characteristics of axial-flow transonic compreseor operating up to tip relative inlet Mach number 1.34 [with list of references]; by John W. R. Creagh.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 17, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

385. NACA research memorandum RM (series). E56E14. Turbojet performance and operation at high altitudes with hydrogen and Jp-4 fuels [with list of references]: by W. A. Fleming [and others].

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 7, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

386. NACA research memorandum RM (series). E56E17. Study of ram-air heat exchangers for reducing turbine cooling-air temperature of supersonic aircraft turbojet engine [with list of references]; by Anthony J. Diaguila, John N. B. Livingood, and Ernst R. G. Eckert.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 3, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

387. NACA research memorandum RM (series). L56F12a. Flight and analytical study of roll requirements of fighter airplane [with list of references]; by James J. Adams.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 3, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

388. NACA research memorandum RM (series). A55F29. Fuselage side inlets, study of some factors affecting their performance and comparison with nose inlets [with list of references]; by Emmet A. Mossman, Frank A. Pfyl, and Frank A. Lazzeroni.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 2, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

389. NACA research memorandum RM (series). L56E30. Exploratory investigation at Mach number of 5.20 of longitudinal aerodynamic characteristics of flat-bottom bodies [with list of references]; by Roy H. Lange.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 27, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

390. NACA research memorandum RM (series). L56E22. Pressure distributions and aerodynamic characteristics of several spoiler-type controls on trapezoidal wing at Mach numbers of 1.61 and 2.01 [with list of references]; by Douglas R. Lord and K. R. Czarnecki.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 26, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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