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

391. NACA research memorandum RM (series). H56E08. Flight-determined transonic lift and drag characteristics of YF-102 airplane with 2 wing configurations [with list of references]: by Edwin J. Saltzman, Donald R. Bellman, and Norman T. Musialowski.

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

392. NACA research memorandum RM (series). L56D30. Free-flight investigation of effects of simulated sonic turbojet exhaust on drag of twin-jet boat-tail bodies at transonic speeds [with list of references]; by Abraham Leiss.

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

393. NACA research memorandum RM (series). L56D25. Free-flight aerodynamic-heating data to Mach number 10.4 for modified Von Karman nose shape [with list of references]; by William M. Bland, jr., and Katherine A. Collie.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 10, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

394. NACA research memorandums RM (series). E56D16. Performance of short turbojet combustor with hydrogen fuel in quarter-annulus duct and comparison with performance in full-scale engine [with list of references]; by Robert Friedman, Cart T. Norgren, and Robert E. Jones.

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

395. NACA research memorandum RM (series). E56C14. External-stream effects on gross thrust and pumping characteristics of ejectors operating at off-design Mach numbers [with list of references]; by Alfred S. Valerino and Richard A. Yeager.

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

396. NACA research memorandum RM (series). E56C08. Analytical and experimental investigation of temperature-schedule acceleration control for turbojet engine [with list of references]; by Herbert Heppler, Paul M. Stiglic and David Novik. Washington.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 22, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

397. NACA research memorandum RM (series). L55F08. Lateral stability and control measurements of fighter-type airplane with low aspect-ratio unswept wing and tee-tail with list of references]; by Donald D. Arabian and James W. Schmeer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 12, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

398. NACA research memorandum RM (series). H56C29. Flight determination of lateral handling qualities of Bell X-5 research airplane at 58.7° sweepback [with list of references]; by Thomas W. Finch and Joseph A. Walker.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

399. NACA research memorandum RM (series). L56C23. Heat transfer on lifting surfaces of 60° delta wing at angle of attack for Mah number 1.98 [with list of references]; by Howard S. Carter.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 31, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

400. NACA research memorandum RM (series). E55K03. Effect of inlet-guide-vane angle on blade vibration and rotating stall of 13-stage axial-flow compressor in turbojet engine [with list of references]; by Howard F. Calvert, Arthur A. Medeiros, and Donald F. Johnson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 22, 1956
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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