Author: National Aeronautics and Space Administration / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

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421. NACA research memorandum RM (series). L57F27. Temperature measurements from flight test of 2 wing-body combinations at 7° angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2x10° [with one reference]; by Leo T. Chauvin.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

422. NACA research memorandum RM (series). L57G16. Effect of ground proximity on aerodynamic characteristics of 2 horizontal-altitude jet vertical-take-off-and-landing airplane models [with list of references]; by William A. Newsom, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

423. NACA research memorandum RM (series). L57G18. Effect of conical and flat sting-mounted windshields on zero-lift drag of flare-stabilized bluff body at Mach numbers from 0.6 to 1.15 [with list of references]; by Willard S. Blanchard, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 12, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

424. NACA research memorandum RM (series). L57G11. Free-flight investigation of jet effect on low-lift drag and longitudinal trim of supersonic interceptor-type airplane configuration with overhanging tail boom at Mach numbers from 1.09 to 1.34 [with list of references]; by Willard S. Bianchard, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 10, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

425. NACA research memorandum RM (series). A57F06b. Effects of wing-tip droop on longitudinal characteristics of 2 highly swept wing-body combinations at Mach numbers from 0.6 to 1.4 [with list of references]; by Earl D. Knechtel and George Lee.

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

426. NACA research memorandum RM (series). E57F03. Effects of internal-area distribution, spike translation, and throat boundary-layer control on performance of double-cone axisymmetric inlet at Mach numbers from 3.0 to 2.0 [with list of references]; by James F. Connors, J. Calvin Lovell, and George A. Wise.

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

427. NACA research memorandum RM (series). L57F19. Free-flight investigation of jet effects at low supersonic Mach numbers on fighter-type configuration employing tall-boom assembly, longitudinal stability and trim [with list of references]; by Bruce G. Jackson and Norman L. Crabill.

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

428. NACA research memorandum RM (series). L57G12. Effects of wing warp on lift, drag, and static longitudinal stability characteristics of aircraft configuration having arrow wing of aspect ratio 1.86 at Mach numbers from 1.1 to 1.7 [with list of references]; by Gillespie, Warren jr.

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

429. NACA research memorandum RM (series). H57G09. Effects of jet exhausts on flight-determined longitudinal and lateral dynamic stability characteristics of Douglas D-558-II research airplane [with list of references]; by Chester H. Wolowicz and Herman A. Rediess.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 23, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

430. NACA research memorandum RM (series). L57E27. Effects of control profile on oscillating hinge-moment and flutter characteristics of flap-type control at transonic speeds [with list of references]; by William C. Moseley, jr., and George W. Price, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 23, 1957
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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