Investigation of the Low-subsonic Stability and Control Characteristics of a 0.34-scale Free-flying Model of a Modified Half-cone Reentry Vehicle
Author: James L. Hassell
Publisher:
Published: 1962
Total Pages: 52
ISBN-13:
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Author: James L. Hassell
Publisher:
Published: 1962
Total Pages: 52
ISBN-13:
DOWNLOAD EBOOKAuthor: James L. Hassell
Publisher:
Published: 1960
Total Pages: 48
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DOWNLOAD EBOOKAuthor: PETER C. BOISSEAU
Publisher:
Published: 1962
Total Pages: 1
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DOWNLOAD EBOOKAn investigation of the low-subsonic flight characteristics of a model having a thick flat 75 degrees swept delta wing with a half-cone fuselage on the upper surface was made in the Langley full-scale tunnel over an angle-ofattack range from about 20 to 40 degrees. Static and dynamic force test data were also obtained. The longitudinal flight characteristics were generally satisfactory over the angle-of-attack range of the investigation. Because of low damping of the Dutch roll oscillation, the lateral stability and control characteristics were poor throughout the angle-of-attack range (20 to 30 degrees) where flights were possible without artificial damping. Artificial damping in roll greatly improved the lateral characteristics so that flights could be made up to an angle of attack of about 40 degrees. (Author).
Author:
Publisher:
Published: 1963
Total Pages: 162
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DOWNLOAD EBOOKAuthor: George M. Ware
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Published: 1960
Total Pages: 20
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DOWNLOAD EBOOKAuthor: James L. Hassell
Publisher:
Published: 1960
Total Pages: 52
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DOWNLOAD EBOOKAuthor: John W. Paulson
Publisher:
Published: 1961
Total Pages: 36
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Publisher:
Published: 1963
Total Pages: 1074
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DOWNLOAD EBOOKLists 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.
Author: John W. Paulson
Publisher:
Published: 1961
Total Pages: 34
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Published: 1966
Total Pages: 1440
ISBN-13:
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