Author: National Aeronautics and Space Administration / Publisher: National Aeronautics and Space Administration - Blacklight Search Results

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16281. 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.)

16282. 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.)

16283. NACA research memorandum RM (series). H58B24. Flight investigation of aerodynamic forces on wing-mounted externalstore installation on Douglas D-558-II research airplane [with list of references]; by Clinton T. Johnson.

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/(letter-nos.)

16284. 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.)

16285. 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.)

16286. 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

16287. NACA research memorandum RM (series). L57L13. Tests of aerodynamically heated multiweb wing structures in free jet at Mach number 2: 4 aluminum-alloy models of 20-inoh chord and span with 0.004-inch-thick skin, 0.025-inch-thick ribs and webs, and zero, 1, 2, or 3 chordwise ribs [with list of references]: by John R. Davidson, Richard Rosecrans, and Louis F. Vosteen.

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/(letter-nos.)

16288. NACA research memorandum RM (series). L58B18. Heat transfer for Mach numbers up to 2.2 and pressure distributions for Mach numbers up to 4.7 from flight investigations of flat-facecone and hemisphere-cone I with list of references]; by Katherine C. Speegle, Leo T. Chauvin, and Jack C. Heberlig.

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/(letter-nos.)

16289. 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

16290. 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.)

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