Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack

Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack
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Total Pages : 42
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ISBN-10 : UOM:39015086490169
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Rating : 4/5 (69 Downloads)

Book Synopsis Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack by : Russell W. McDearmon

Download or read book Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack written by Russell W. McDearmon and published by . This book was released on 1956 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental values of the damping in roll of three triangular wings have been obtained at Mach numbers of 1.62, 1.94, 2.22, 2.41, and 2.62 over a range of angle of attack from approximately 0 to 13 degrees. The aspect ratios of the wings were 1.46, 2.31, and 3.35.


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