The Effect of High Wing Loading on Landing Technique and Distance, with Experimental Data for the B-26 Airplane PDF Download
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Author: F. B. Gustafson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 112
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Book Description
1. Considerations of safety and accuracy limit the rate of descent used in the landing approach to about 25 feet per second.
Author: F. B. Gustafson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 112
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Book Description
1. Considerations of safety and accuracy limit the rate of descent used in the landing approach to about 25 feet per second.
Author: Langley Aeronautical Laboratory
Publisher: Hassell Street Press
ISBN: 9781014962751
Category :
Languages : en
Pages : 104
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Book Description
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 400
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 712
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 332
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Book Description
Author: Vernon H. Gray
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 720
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Book Description
The effects of primary and runback icing and frost formations on the drag of an 8-foot-chord NACA 651-212 airfoil section were investigated over a range of angles of attack from 2 degrees to 8 degrees and airspeeds up to 260 miles per hour for icing conditions with liquid-water contents ranging from 0.25 to 1.4 grams per cubic meter and datum air temperatures of -30 to 30 degrees F.
