Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack PDF full book. Access full book title Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack by Russell W. McDearmon. Download full books in PDF and EPUB format.
Author: Russell W. McDearmon Publisher: ISBN: Category : Airplanes Languages : en Pages : 42
Book Description
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.
Author: Russell W. McDearmon Publisher: ISBN: Category : Airplanes Languages : en Pages : 42
Book Description
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.
Author: Russell W. McDearmon
Author: Russell W. McDearmon
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: 
Author: United States. National Aeronautics and Space Administration
Author: 
Author: United States. National Aeronautics and Space Administration
Author: 
Author: 
Author: Defense Documentation Center (U.S.)