Catalog Issue Year Decade: 1960 - 1969 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Catalog Issue Year Decade 1960 - 1969 Sudoc Stem Y 3.N 21/5

71. NACA research memorandum RM (series). L58F06. Experimental investigation of 2 internal-compression air-inlet designs which use fluid boundaries as means of supersonic compression [with list of references]; by Robert R. Howell and Charles D. Trescot, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 14, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

72. NACA research memorandum RM (series). L58E07a. Preliminary studies of manned satellites, wingless configuration, nonlifting [with list of references]; by Maxine A. Faget, Benjamine J. Garland, and James J. Buglia.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 11, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

73. NACA research memorandum KM (series). SL58H07. Free-spinning-tunnel investigation of 1/28-scale model of North American FJ-4 airplane with external fuel tanks, TED no. NACA AD 3112 [with list of references]; by Frederick M. Healy.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [Aug. 8, 1958.]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

74. NACA research memorandum RM (series). E58D03a. Study of combustion rates of hydrocarbon fuels with red fuming nitric acid in small rocket engine [with list of references]; by Louis Baker, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 6, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

75. NACA research memorandum RM (series). L58F02. Wind-tunnel investigation of low-speed stability and performance characteristics of jet-powered low-aspect-ratio vertical-take-off-and landing configuration with engines buried in tiltable wings [with list of references]; by William I. Scallion and Clarence D. Cone.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 6, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

76. NACA research memorandum RM (series). A58E05. Flight investigation of low-speed characteristics of 45° swept-wing fighter-type airplane with blowing boundary-layer control applied to trailing-edge flaps [with list of references]; by Hervey C. Quigley, Seth B. Anderson, and Robert C. Innis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

77. NACA research memorandum RM (series). L58E21. Aerodynamic characteristics at Mach nos. 2.36 and 2.87 of airplane configuration having cambered arrow wing with 75° swept leading edge [with list of references]; by Joseph M. Hallissy, jr., and Dennis F. Hasson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Aug. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

78. NACA research memorandum RM (series). E58D03. Chemical and physical factors affecting combustion in fuel-nitric acid systems [with list of references]; by Louis Baker, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 28, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

79. NACA research memorandum RM (series). H58D21. Operational problems of manned orbital vehicles; by Hubert M. Drake, Donald R. Bellman, and Joseph A. Walker.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 21, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

80. NACA research memorandum RM (series). L58C27. Investigation of aerodynamic characteristics of model of supersonic bomber configuration with swept and unswept wing at Mach numbers from 1.79 to 2.67; by H. Norman Silvers and Raymond L. Zedekar.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: July 21, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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