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

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17291. NACA research memorandum RM (series). E52I02. Influence of fuselage-mounted rocket boosters on flow field at inlet and on diffuser performance of strut-mounted engine at Mach numbers of 1.8 and 2.0 [with one reference]; by George A. Wise and Leonard J. Obery.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 29, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17292. NACA research memorandum RM (series). E52H12. Performance characteristics of 1 convergent and 3 convergent-diver gent nozzles [with list of references] by H. George Krull and Fred W. Steffen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 29, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17293. NACA research memorandum RM (series). L52G01. Investigation of several supersonic missile configurations directed toward minimising center-of-pressure travel [with list of references]; by Robert W. Ralnev.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 23, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17294. NACA research memorandum RM (series). L52E00b. Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds [with list of references]: by Paul E. Purser and Jesse L. Mitchell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Sept. 15, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17295. NACA research memorandum RM (series). E52G29. Altitude investigation of 3 flame-holder and fuel-systems configurations in short converging afterburner on turbojet engine [with list of references]; by Willis M. Braithwaite, Paul E. Renas, and Emmert T. Jansen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 10, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17296. NACA research memorandum RM (series). E52G30. Investigation of thrust augmentation using water-alcohol injection on 5200-pound-thrust axial-flow-type turbojet engine at static sealevel conditions [with list of references]; by David S. Boman and William E. Mallett.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 4, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17297. NACA research memorandum RM (series). A52E23. Effects of simulated skin wrinkles of wing surface on aerodynamic characteristics of 2 wing-body combinations employing wings of low aspect ratio at subsonic and supersonic speeds [with list of references]; by John C. Heitmeyer and Willard G. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 5, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17298. NACA research memorandum RM (series). E52F09. Performance characteristics of normal-shock side inlet located downstream of canard control surface at Mach numbers of 1.5 and 1.8 [with list of references]; by Murray Dryer and Andrew Beke.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 29, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17299. NACA research memorandum RM (series). L52E02a. Investigation of supersonic aircraft configuration having tapered wing with circular-arc sections and 40° sweepback, pressure-distribution measurements of interference effect of wing on fuselage at Mach numbers of 1.40 and 1.59 [with list of reference]; by John P. Gapcynski and James W. Clark.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 17, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17300. NACA research memorandum RM (series). E52E13. Influence of canard-type control surface on flow field in vicinity of symmetrical fuselage at Mach numbers 1.8 and 2.0 [with list of references]; by George A. Wise and Murray Drver.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 16, 1952
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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