The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50°
Author: John B. McDevitt
Publisher:
Published: 1960
Total Pages: 114
ISBN-13:
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Author: John B. McDevitt
Publisher:
Published: 1960
Total Pages: 114
ISBN-13:
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Publisher:
Published: 1966
Total Pages: 108
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DOWNLOAD EBOOKAuthor: John B. McDevitt
Publisher:
Published: 1960
Total Pages: 104
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DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1963
Total Pages: 76
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DOWNLOAD EBOOKAuthor: Mitchel H. Bertram
Publisher:
Published: 1954
Total Pages: 58
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DOWNLOAD EBOOKA program to investigate the aerodynamic characteristics of a family of delta wings with a blunt double-wedge section has been conducted at the Langley 11-inch hypersonic tunnel. These wings had a maximum thickness of 8 percent of the chord located at the 18-percent-chord point. For the wings tested at a Mach number of 6.9, the semiapex angle was varied from 5 to 30 degrees and the wings were tested over a range of angle of attack from 0 to 28 degrees and Reynolds numbers in the range of 800,000 to 3,600,000 based on root chord. In addition, pertinent results from tests at Mach number as low as 1.62 have been utilized. The shock-expansion theory and the Newtonian impact theory have been used to analyze the effects of changes made in the various parameters investigated.
Author: Dewey E. Wornom
Publisher:
Published: 1964
Total Pages: 30
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DOWNLOAD EBOOKAuthor: Emma Jean Landrum
Publisher:
Published: 1962
Total Pages: 76
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DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Published: 1967
Total Pages: 2300
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Published: 1995
Total Pages: 704
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DOWNLOAD EBOOKAuthor: Robert W. Dunning
Publisher:
Published: 1953
Total Pages: 24
ISBN-13:
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