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

401. NACA research memorandum RM (series). E57F13. Internal performance of several divergent-shroud ejector nozzles with high-divergence angles [with list of references]; by Arthur M. Trout, S. Stephen Papell, and John H. Povolny.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 2, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

402. NACA research memorandum RM (series). E57G25a. Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet [with list of references; by Milton A. Beheim and Thomas G. Piercy.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 2, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

403. NACA research memorandum RM (series). L57F13. Flight investigation of factors affecting choice of minimum approach speed for carrier-type landings of swept-wing jet fighter airplane [with list of references]; by Lindsay J. Lina, Garland J. Morris, and Robert A. Champine.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 30, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

404. NACA research memorandum RM (series). L57G25. Lateral stability investigation at Mach numbers from 0.8 to 1.7 of 2 rocket-boosted models of airplane configuration with 45° swept wing and low horizontal tail [with list of references]; by John C. McFall, Jr., Jesse L. Mitchell, and A. James Vitale.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 30, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

405. NACA research memorandum RM (series). L57H0S. Transonic Investigation of axial-flow compressor rotor with hub-tip ratio of 0.75 and blades having NACA A2I8b mean lines [with list of references]: by Peter T. Bernot and Melvyn Savage.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 30, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

406. NACA research memorandum RM (series). A57G10. Flight investigation of low-speed characteristics of 35° swept-wing airplane equipped with area-suction ejector flap and various wing leading-edge devices [with list of references]; by Seth B. Anderson, Alan E. Faye. jr., and Robert C. Innis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 26, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

407. NACA research memorandum RM (series). L57G08. Investigation of screens for removing distortions in ducted flows at high subsonic speeds; [with list of references]; by Charles C. Wood and Gerald Knip, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 26, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

408. NACA research memorandum RM (series). L57G09a. Investigation at transonic speeds of loading over 30° sweptback wing of aspect ratio 3, taper ratio 0.2, and NACA 65A004 airfoil section mounted on body [with list of references]; by Donald D. Arabian.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 26, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

409. NACA research memorandum RM (series). L57G10. Comparison of low-lift drag at Mach numbers from 0.74 to 1.37 of rocket-boosted models having externally braced wings and cantilever wings [with list of references]; by Waldo L. Dickens and Earl C. Hastings, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 25, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

410. NACA research memorandum RM (series). L57G17. Transonic investigation of effects of spanwise and chordwise external store location and body contouring on aerodynamic characteristics of 45° sweptback wing-body configurations [with list of references]; by Albin O. Pearson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 25, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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