Publish Year Decade: 1960 - 1969 / Sudoc Stem: NAS 1.15 - Blacklight Search Results

Start Over Publish Year Decade 1960 - 1969 Sudoc Stem NAS 1.15

81. NASA technical memorandum TM (series). X-275. Pressure distribution of 0.0667-scale model of X-15 airplane for angle-ofattack range of 0° to 28° at Mach numbers of 2.30, 2.88, and 4.65 [with list of references]; by B. Leon Hodge and Paige B. Burbank.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 1960
SuDoc number:: NAS 1.15:X-(nos.)

82. NASA technical memorandums. X-239. Fin loads and tip-control hinge moments on ⅛-scale model simulating 1st stage of Scout research vehicle at Much number of 2.01: by Ross B. Robinson and Emma Jean Landrum.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 1960
SuDoc number:: NAS 1.15:X-(nos.)

83. NASA technical memorandums. X-240. Hypersonic longitudinal trim, stability, and control characteristics of delta-wing configuration at high angles of attack [with list of references]; by William H. Close.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 1960
SuDoc number:: NAS 1.15:X-(nos.)

84. NASA technical memorandums. X-249. Aerodynamic and hydrodynamic characteristics of proposed supersonic multijet water-based hull-type airplane with variable-incidence wing [with list of references]; by William W. Petvnia, Albin O. Pearson, and Roger H. Fournier.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 1960
SuDoc number:: NAS 1.15:X-(nos.)

85. NASA technical memorandums. X-271. Aerodynamic characteristics of model of proposed 6-engine hull-type seaplane at Mach numbers of 1.57, 1.87. and 2.16 [with list of references]: by James R. Morgan and Ann B. Fichter.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 1960
SuDoc number:: NAS 1.15:X-(nos.)

86. NASA technical memorandums. X-273. Effects of spoiler-slot deflector control on aerodynamic characteristics at Mach number of 2.01 of variable-wing-sweep configuration with outer wing panels swept back 75° [with list of references]: by Gerald V. Foster.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 1960
SuDoc number:: NAS 1.15:X-(nos.)

87. NASA technical memorandums. X-361. Wind-tunnel investigation of static and dynamic-rotnry stability derivatives of flat-top wing-hody model at Mach numbers of 2.5, 3.0, and 3.5 [with list of references]; by Bedford A. Lampkin and Kenneth C. Endicott.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Apr. 1960
SuDoc number:: NAS 1.15:X-(nos.)

88. NASA technical memorandum. X-85. Cascade investigation of cooling characteristics of corrugated-insert aircooled turbine blade for use in turboprop engine [with list of references]; by Hadley T. Richards.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 1960
SuDoc number:: NAS 1.15:X-85

89. NASA technical memorandums. X-151. Mixing characteristics downstream of core region of high-temperature axisymmetric jets exhausting into transonic and supersonic streams [with list of references]; by Ronald G. Huff and Kaleel L. Abdalla.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 1960
SuDoc number:: NAS 1.15:X-(nos.)

90. NASA technical memorandums. X-208. Heat transfer to 36.75° and 45° swept blunt leading edges in free flight at Much numbers from 1.70 to 2.99 and from 2.50 to 4.05 [with list of references]; by Robert L. O'Neal.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 1960
SuDoc number:: NAS 1.15:X-(nos.)

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