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

271. NACA technical notes. 4301. Errata [Effects of boundary-layer displacement and leading-edge bluntness on pressure, distribution, skin friction, and heat transfer of bodies at hypersonic speeds], by Mitchel H. Bertram and Arthur Henderson, jr., June 1958.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 8, 1958
SuDoc number:: Y 3.N 21/5:6/4301/errata

272. Reports (1957). 1321. Errata, Theoretical calculation of power spectra of rolling and yawing moments on wing in random turbulence, by John M. Eggleston and Franklin W. Diederich.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [May 8, 1958.]
SuDoc number:: Y 3.N 21/5:(nos.)

273. NACA research memorandum RM (series). A58A31. Effect of moment-of-area-rule modifications on zero-lift drag of 3 wing-body combinations [with list of references]; by Robert R. Dickey.

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.)

274. NACA research memorandum RM (series). E57H28. Experimental results of investigation of 2 methods of inflight thrust measurement applicable to afterburning turbojet engines with ejectors [with list of references]; by Harry E. Bloomer.

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.)

275. 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.)

276. Technical notes. 4242. General solutions for flow past slender cambered wings with swept trailing edges and calculation of additional loading due to control surfaces [with list of references]; by E. B. Klunker and Keith C. Harder.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

277. Technical notes. 4247. Study of ground-reaction forces measured during landing impacts of large airplane [with list of references]; by Albert W. Hall, Richard H. Sawyer, and James M. McKay.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

278. Technical notes. 4248. Summary of experimental heat-transfer measurements in turbulent flow for Mach number range from 0.87 to 5.05 [with list of references]; by Maurice J. Brevoort and Barbara D. Arabian.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

279. Technical notes. 4251. Experimental investigation of wake effects on hydro-skis [with list of references]; by Ellis E. McBride and Lloyd J. Fisher.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

280. Technical notes. 4254. Flight investigation of effects of retreating-blade stall on bending and torsional moments encountered by helicopter rotor blade [with list of references]; by LeRoy H. Ludi.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: May 1958
SuDoc number:: Y 3.N 21/5:6/(nos.)

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