Item Details

Static Aerodynamic Characteristics, Pressure Distributions, and RAM-Air Inflation of Attached Inflatable Decelerator Models at Mach 3.0

William D. Deveikis and James Wayne Sawyer
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970.
Language
English
Variant Title
NASA TN D-5816
Series
NASA Technical Note
SuDoc Number
NAS 1.14:D-5816
Summary
Static aerodynamic characteristics, pressure distributions, and ram air inflation of attached inflatable drag chute models at supersonic speed.
Description
59 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
Includes bibliographical references (p. 19).
Series Statement
NASA technical note ; D-5816
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Static aerodynamic characteristics, pressure distributions, and RAM-air inflation of attached inflatable decelerator models at Mach 3.0 / c| William D. Deveikis and James Wayne Sawyer.
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    a| NASA technical note ; v| D-5816
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    a| Includes bibliographical references (p. 19).
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    a| Static aerodynamic characteristics, pressure distributions, and ram air inflation of attached inflatable drag chute models at supersonic speed.
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    a| Mode of access: Internet.
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    a| Wind tunnels x| Testing.
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    a| Aerodynamics, Supersonic.
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