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

1201. NACA research memorandum RM (series). E53E06. Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics: 2, Effect of compressor interstage air bleed [with list of references]; by John J. Rebeske, jr. and James F. Dugan, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 3, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1202. NACA research memorandum RM (series). L53E18a. Discussion of 3-dimensional oscillating air forces based on windtunnel measurements [with list of references]; by Sherman A. Clevenson, Summer A. Leadbetter and Weimer J. Tuovilla., .

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 30, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1203. NACA research memorandum RM (series). E53D22. Altitude performance investigation of high-temperature afterburner [with list of references]; by S. C. Huntley, Carmon M. Auble, and James W. Useller.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 26, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1204. NACA research memorandum RM (series). L53D22. Preliminary results from limited investigation of use of controls during service operational training with fighter airplanes [with list of references]; by John P. Mayer, Carl R. Huss, and Harold A. Hamer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 16, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1205. NACA research memorandum RM (series). A53D02. Experimental investigation of zero-lift drag of fin-stabilized body of fineness ratio 10 at Mach numbers between 0.6 and 10 [with list of references]; by Carlton S. James and Robert J. Carros.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 11, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1206. NACA research memorandum RM (series). L53D30a. Aerodynamic characteristics of 2 delta wings and 2 trapezoidal wings at Mach number 4.04 [with list of references]; by Robert W. Dunning and Fred M. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 11, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1207. NACA research memorandum RM (series). L53D13. Effects of trailing-edge bluntness on lift, drag, and pitching-moment characteristics of unswept, 45° swept, and 45° delta wings at Mach numbers of 1.41, 1.62, and 1.96 [with list of references]; by Kennith L. Goln and Gertrude C. Westrick.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 10, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1208. NACA research memorandum RM (series). E53D07. Investigation at Mach number of 1.90 of diverter-type boundary-layer removal system for scoop inlet [with list of references]: by Fred D. Kochendorfer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 8, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1209. NACA research memorandum RM (series). L53E08. Summary of data on division of loads for various wing-fuselage combinations [with list of references]; by Clarence L. Gillis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 8, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1210. NACA research memorandum RM (series). L53D16. Loads experienced in flights of 2 swept-wing research airplanes in angle-of-attack range of reduced stability [with list of references]; by Hubert M. Drake, Glenn H. Robinson, and Albert E. Kuhl.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: June 5, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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