Publish Year Decade: 1950 - 1959 / Catalog Issue Year Decade: 1960 - 1969 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Catalog Issue Year Decade 1960 - 1969

101. NASA memorandums. 10-1-58A. Effects of longitudinal control-system dynamics on pilot opinion and response characteristics as determined from flight tests and from ground simulator studies [with list of references]; by Melvin Sadoff.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1958
SuDoc number:: NAS 1.10:(nos.)

102. NASA memorandums. 10-1-58L. Longitudinal and lateral stability and control characteristics of various combinations of component parts of 2 canard airplane configurations at Mach numbers of 1.41 and 2.01 [with list of references]; by Cornelius Driver.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1958
SuDoc number:: NAS 1.10:(nos.)

103. NASA memorandums. 10-11-58L. Aerodynamic characteristics in sideslip of large-scale 49° sweptback wing-body-tail configuration with blowing applied over flaps and wing leading edge [list list of references]; by H. Clyde Me-Lemore.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1958
SuDoc number:: NAS 1.10:(nos.)

104. NASA memorandums. 10-12-58L. Tests of aerodynamically heated multiweb wing structures in free jet at Mach number 2: Three models of 20-inch chord and span constructed from magnesium, titanium, and aluminum alloys, respectively [with list of references]; by John R. Davidson and Richard Rosecrans.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1958
SuDoc number:: NAS 1.10:(nos.)

105. NASA memorandums. 10-2-58L. Aerodynamic characteristics for combined angles of attack and sideslip of low-aspect-ratio cruciform-wing missile configuration employing various canard and trailing-edge flap controls at Mach number of 2.01 [with list of references]; by Ross B. Robinson and M. Leroy Spearman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1958
SuDoc number:: NAS 1.10:(nos.)

106. NASA memorandums. 10-3-58L. Wind-tunnel investigation of some effects of wing sweep and horizontal-tail height on static stability of airplane model at transonic speeds [with list of references]; by Lewis R. Fisher and James L. Williams.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1958
SuDoc number:: NAS 1.10:(nos.)

107. NASA memorandums. 10-5-58L. Some effects of horizontal-tail position on vertical-tall pressure distributions of complete model in sideslip at high subsonic speeds [with list of references]; by William J. Alford, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1958
SuDoc number:: NAS 1.10:(nos.)

108. Petroleum products survey (series). 6. Burner fuel oils, 1958; prepared by O. C. Blade.

Corporate/Agency Authors:: Mines Bureau and Interior Dept.
Publisher:: Mines Bureau
Date:: Oct. 1958
SuDoc number:: I 28.18/3:(nos.)

109. Photo series. 23. Processing ready-to-cook fryer chickens, n.p.

Corporate/Agency Authors:: Agriculture Department
Publisher:: Agriculture Department
Date:: Oct. 1958
SuDoc number:: A 1.100/2:(nos.)

110. Photo series. 24. Processing turkeys, California, n.p.

Corporate/Agency Authors:: Agriculture Department
Publisher:: Agriculture Department
Date:: Oct. 1958
SuDoc number:: A 1.100/2:(nos.)

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