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

261. NACA research memorandum RM (series). E57K25a. Method for determining turbine design characteristics for rocket turbodrive applications [with list of references]; by Warner L. Stewart, David G. Evans, and Warren J. Whitney.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 2, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

262. NACA research memorandum RM (series). L58B25. Effect of control trailing-edge thickness or aspect ratio on oscillating hinge-moment and flutter characteristics of flap-type control at transonic speeds [with list of references]; by William C. Moseley, jr., and Robert F. Thompson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 23, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

263. NACA research memorandum RM (series). A57K07. Analytical evaluation of effects of aerodynamic modification and of stability augmenters on pitch-up behavior and probable pilot opinion of 2 current fighter airplanes [with list of references); by Melvin Sadoff and John D. Stewart.

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

264. NACA research memorandum RM (series). H58A30. Analysis of surface pressures and aerodynamic load distribution over swept wing of Douglas D-558-II research airplane at Mach numbers from 0.73 to 1.73 [with list of references]; by Norman V. Taillon.

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

265. NACA research memorandum RM (series). L58B04. Free-flight investigation to determine inlet external drag of 4 inlet models at Mach numbers from 1.50 to 3.00 [with list of references]; by Walter L. Kouyoumjian.

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

266. NACA research memorandum RM (series). L58B19. Effect of compressibility on hovering performance of two 10-foot-diameter helicopter rotors tested in Langley full-scale tunnel [with list of references]; by Joseph W. Jewel, jr., and Robert D. Harrington.

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

267. NACA research memorandum RM (series). L58A31. Effects of shock-boundary-layer interaction on performance of long and short subsonic annular diffuser [with list of references]; by Charles C. Wood and John R. Henry.

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

268. NACA research memorandum RM (series). A58A14. Wind-tunnel data on longitudinal and lateral-directional rotary derivatives of straight-wing, research airplane configuration at Mach numbers from 2.5 to 8.5 [with list of references]; by Benjamin H. Beam and Kenneth C. Endicott.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 25, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

269. NACA research memorandum RM (series). L57K22. Feasibility of nose-cone cooling by upstream ejection of solid coolants at stagnation point [with list of references]; by William H. Kinard.

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.)

270. NACA research memorandum RM (series). L58A13. Heat transfer to 0° and 75° swept blunt leading edges in free flight at Mach numbers from 1.90 to 3.07 [with list of references]; by Robert L. O'Neal and Aleck C. Bond.

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.)

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