Author: National Aeronautics and Space Administration / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Sudoc Stem Y 3.N 21/5

271. NACA research memorandum RM (series). L58B06. Preliminary study of airplane configurations having tall surfaces outboard of wing tips [with list of references]; by William C. Sleeman, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

272. NACA research memorandum RM (series). L58B07. Aerodynamic characteristics of canard and outboard-tall airplane model at Mach number of 2.01 [with list of references]; by M. Leroy Spearman and Ross B. Robinson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 24, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

273. NACA research memorandum RM (series). E57K26. Aerodynamic and inlet-flow-field characteristics at free-stream Mach numher of 3.0 for airplanes with circular fuselage cross sections [with list of references]; by Murray Dryer and Roger W. Luidens.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 18, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

274. NACA research memorandum RM (series). L57L10. Calculation of flutter characteristics for finite-span swept or onswept wines at subsonic and supersonic speeds by modified strip analysis (with list of references]; by E. Carson Yates, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 18, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

275. NACA research memorandum RM (series). L58A22. Preliminary investigation of land-water operation with 1/10-scale model of jet airplane equipped with hydro-skis [with one reference]; by William C. Thompson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 18, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

276. NACA research memorandum RM (series). A57K21. Analog study of influence of internal modifications to wing leading edge on its transient temperature rise during high-speed flight [with list of references]; by Carr B. Neel.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

277. NACA research memorandum RM (series). L58A02. Two-dimensional cascade investigation at Mach numbers up to 1.0 of NACA 65-series blade sections at conditions typical of compressor tips [with list of references]; by James C. Dunavant and James C. Emery.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

278. NACA research memorandum RM (series). L58A03. Section thrust coefficients for full-scale, 3 blade, supersonic-type propeller operating at low and negative blade angles [with list of references]; by Leland B. Salters, jr., and Martha C Lewis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Mar. 17, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

279. NACA research memorandum RM (series). A58A08. Experimental lift-drag ratios for 2 families of wing-body combinations at supersonic speeds [with list of references]; by Leland H. Jorgensen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 10, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

280. NACA research memorandum RM (series). L58A20. Longitudinal and lateral stability and control characteristics at Mach no. 2.01 of 60° delta-wing airplane configuration equipped with canard control and with wing tralling-edge flap controls [with list of references]; by M. Leroy Spearman and Cornelius Driver.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 10, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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