Flight Tests at Transonic and Supersonic Speeds of an Airplane-like Configuration with a Thin Straight Sharp-edge Wings and Tail Surfaces
Author: Clarence L. Gillis
Publisher:
Published: 1949
Total Pages: 44
ISBN-13:
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Author: Clarence L. Gillis
Publisher:
Published: 1949
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1959
Total Pages: 388
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1957
Total Pages: 388
ISBN-13:
DOWNLOAD EBOOKAuthor: Joseph Adams Shortal
Publisher:
Published: 1978
Total Pages: 796
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DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1956
Total Pages: 716
ISBN-13:
DOWNLOAD EBOOKAuthor: Paul E. Purser
Publisher:
Published: 1952
Total Pages: 26
ISBN-13:
DOWNLOAD EBOOKSome approximate values of the yawing moment due to sideslip derivative for eight airplane-like configurations flown as rocket models for other purposes, at transonic speeds, have been collected and compared with the available subsonic and supersonic wind-tunnel data for the same configurations.
Author: Clarence L. Gillis
Publisher:
Published: 1948
Total Pages:
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DOWNLOAD EBOOKAuthor: Charles T. D'Aiutolo
Publisher:
Published: 1950
Total Pages: 36
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DOWNLOAD EBOOKAuthor: Macon C. Ellis
Publisher:
Published: 1949
Total Pages: 44
ISBN-13:
DOWNLOAD EBOOKResults from a supersonic wind-tunnel investigation of a series of thin triangular and sweptback wings are presented. The triangular wing series consisted of eight triangular wings of vertex angles such that a range of leading-edge postions both inside and outside the Mach cone at the test Mach numbers of 1.43 and 1.71 was obtained. The three swept wings had angles of sweep at 45, 55, and 63 degrees and were tested at a Mach number of 1.43.
Author: Peter C. Boisseau
Publisher:
Published: 1961
Total Pages: 54
ISBN-13:
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