Author : Russell W. McDearmon
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
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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 : United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Author :
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494
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Author : United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Author :
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 818
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Author : United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author :
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
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Author :
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 464
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Author : Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1116
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Author : United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 292
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Book Description
Author: Russell W. McDearmon
Author: United States. National Aeronautics and Space Administration
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: United States. National Aeronautics and Space Administration
Author: 
Author: 
Author: Defense Documentation Center (U.S.)
Author: United States. National Aeronautics and Space Administration