Publish Year Decade: 1950 - 1959 / Catalog Issue Year Decade: 1960 - 1969 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Catalog Issue Year Decade 1960 - 1969

271. AEC research reports. 1TR-1502. Operation plumbbob preliminary report, Nevada test site. May 9164 Oct. 1957, civil effects test group: Project 89.3. Thermal radiation measurements (pts. 1 and 9) [with lists of references; by A. L. Greig and Herman E. Pearse].

Corporate/Agency Authors:: Atomic Energy Commission
Publisher:: Atomic Energy Commission
Date:: May 23, 1958
SuDoc number:: Y 3.At 7:22/(letters-nos.)

272. NAVORD reports. 6120. Use Of electrical resistivity in study of polymerisation of thermosetting resins [with list of references]; prepared by B. W. Warfield and M. C. Petree.

Corporate/Agency Authors:: Ordnance Bureau (Navy) and Defense Dept.
Publisher:: Ordnance Bureau (Navy)
Date:: [May 23, 1958.]
SuDoc number:: D 215.7:(nos.)

273. NACA research memorandum RM (series). E58B13. Performance at Mach numbers 3.07, 1.89, and 0 of inlets designed for inlet-engine matching up to Mach 3 [with one reference]; by L. W. Gertsma and M. A. Beheim.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 20, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

274. NACA research memorandum RM (series). E58B24. Relation between flow range and other compressor-stage characteristics [with list of references]; by Arthur W. Goldstein and Ralph L. Schacht.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 20, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

275. NACA research memorandum RM (series). E58B27. Investigation of 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study: 4, Rotor loss patterns as determined by hot-wire anemometers with rotor operating in circumferentially uniform inlet flow field [with list of references]; by Milton O. Kofskey and Hubert W. Allen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 20, 1958
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

276. NACA research memorandum RM (series). L58C10. Some effects of roughness on stagnation-point heat transfer at Mach no. 2, stagnation temperature of 3,530° F, and Reynolds no. 2.5 x 10° per foot [with list of references]; by H. Kurt Strass and Thomas W. Tyner.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 20, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

277. NACA research memorandum RM (series). A58C05. Static stability and control characteristics of triangular wing and canard configuration at Mach numbers from 2.58 to 3.53 [with list of references]; by C. Ernest Hedstrom, James R. Blackabv, and Victor L. Peterson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 13, 1958
SuDoc number:: Y 3.N 21/5:15/(letters-nos.)

278. NACA research memorandum RM (series). E57L19. Preliminary survey of possible cooling methods for hypersonic aircraft [with list of references]; by Jack H. Esgar, Robert O. Hickel, and Francis S. Stepka.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 12, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

279. NACA research memorandum RM (series). E58A27b. Investigation of underslung half-cone inlet with compression surface mounted outboard from fuselage at Mach numbers of 1.5, 1.8, and 2.0 [with list of references]; by Richard A. Yeager and Laurence W. Gertsma.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 12, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

280. NACA research memorandum RM (series). E58C12. Performance of basic XJ79-GE-1 turbojet engine and its components 11400 [with list of references]; by Carl E. Campbell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 8, 1958
SuDoc number:: Y 3.N 21/5:15/E 58 C 12

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