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

291. NACA research memorandum RM (series). L57K21. Study of exit phase of flight of very high altitude hypersonic airplane by means of pilot-controlled analog computer [with list of references]; by Windsor L. Sherman, Stanley Faber, and James B. Whitten.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

292. NACA research memorandum RM (series). L57L18a. Investigation at Mach nos. 1.94 and 2.41 of jet effects upon longitudinal and directional stability of general aircraft configuration employing wing-tip-mounted nacelles [with list of references]; by Frank L. Clark and Clyde L. W. Edwards.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

293. NACA research memorandum RM (series). A57L10. Flight study of longitudinal-control-system dynamic characteristics by use of variable-control-system airplane [with list of references]; by Narman M. McFadden, Frank A. Pauli, and Donovan R. Heinle.

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

294. NACA research memorandum RM (series). L57J28a. Investigation of static lateral stability and aileron characteristics of 0.067-scale model of Bell X-2 airplane at Mach numbers 2.29, 2.78, 3.22, and 3.71 [with list of references]; by Roger H. Fournier and H. Norman Silvers.

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

295. NACA research memorandum RM (series). L57L10a. Investigation at transonic speeds of fixed divergent ejector installed in single-engine fighter model [with list of references]; by John M. Swihart and Charles E. Mercer.

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

296. NACA research memorandum RM (series). E57L12a. Comparison of experimentally and analytically determined windmilling characteristics of compressor with low over-all pressure ratio [with list of references);by James E. Hatch.

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

297. NACA research memorandum RM (series). L57K26. Behavior of some materials and shapes in supersonic free jets at stagnation temperatures up to 4,210° F, and descriptions of jets [with list of references]; by E. M. Fields [and others].

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

298. NACA research memorandum RM (series). L57L17. Experimental determination of effects of frequency and amplitude of oscillation on roll-stability derivatives for 60° delta-wing airplane model [with list of references]; by Lewis K. Fisher.

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

299. NACA research memorandum RM (series). L57H13. Buffet tests of attack-airplane model with emphasis on analysis of data from wind-tunnel tests [with list of references]; by Don D. Davis, jr., and Deewey E. Wornom.

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

300. NACA research memorandum RM (series). L57J22. Tabulated pressure data for 60° delta-wing-body-tail model with hot jet exhausting from pylon-mounted nacelle [with list of references]; by Edwin E. Lee, jr., and John M. Swihart.

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

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