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Aerodynamics, missiles and space vehicles

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1.
A 1-foot hypervelocity shock tunnel in which high-enthalpy, real-gas air flows can be generated with flow times of about 180 milliseconds / Bernard E. Cunningham and Samuel Kraus
Author
Cunningham, Bernard E.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
2.
Effects of surface recombination on heat transfer to bodies in a high enthalpy stream of partially dissociated nitrogen
Author
Winkler, Ernest L.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961 ]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
3.
Ballistic range measurements of stagnation-point heat transfer heat transfer in air and carbon dioxide at velocities up to 18,000 feet per second
Author
Yee, Layton
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1961]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
4.
Measurements of flow duration in a low-pressure shock tube
Author
Sandborn, Virgil A.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
5.
Experimental study of the effects of weightlessness on the configuration of mercury and alcohol in spherical tanks
Author
Petrash, Donald A.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
6.
Design and calibration of an arc-heated, hypersonic, low-density wind tunnel
Author
Weitmann, Ruth N.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
7.
Determining inertias by using the amplitude decay rate of a mechanical oscillating system
Author
Carpenter, Gene T.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online