A Wind Tunnel Investigation At Subsonic And Low Supersonic Speeds Of A Re Entry Vehicle With Retractable Wings PDF Download

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Wind-tunnel Investigation at High Subsonic Speed of the Static Longitudinal Stability Characteristics of a Winged Reentry Vehicle Having a Large Negatively Deflected Flap-type Control Surface

Wind-tunnel Investigation at High Subsonic Speed of the Static Longitudinal Stability Characteristics of a Winged Reentry Vehicle Having a Large Negatively Deflected Flap-type Control Surface
Author: Paul G. Fournier
Publisher:
Total Pages: 24
Release: 1959
Genre: Aerodynamics
ISBN:
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NASA Technical Note

NASA Technical Note
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 994
Release: 1962
Genre: Aeronautics
ISBN:
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Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane - Lateral and Directional Stability

Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane - Lateral and Directional Stability
Author: Benton E. Wetzel
Publisher:
Total Pages: 25
Release: 1955
Genre:
ISBN:
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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author:
Publisher:
Total Pages: 1126
Release: 1987
Genre: Aeronautics
ISBN:
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.