Tests in the Variable-density Wind Tunnel Related Airfoils Having the Maximum Camber Unusually Far Forward PDF Download
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Author: A. M. Rothrock
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 194
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Book Description
Author: A. M. Rothrock
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 194
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 642
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Book Description
Author: James R. Hansen
Publisher: Government Printing Office
ISBN: 9780160831560
Category : Business & Economics
Languages : en
Pages : 990
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Book Description
The airplane ranks as one of history's most ingenious and phenomenal inventions. It has surely been one of the most world changing. How ideas about aerodynamics first came together and how the science and technology evolved to forge the airplane into the revolutionary machine that it became is the epic story told in this six-volume series, The Wind and Beyond: A Documentary Journey through the History of Aerodynamics in America. Following up on Volume I's account of the invention of the airplane and the creation of the original aeronautical research establishment in the United States, Volume II explores the airplane design revolution of the 1920s and 1930s and the quest for improved airfoils. Subsequent volumes cover the aerodynamics of airships, flying boats, rotary-wing aircraft, breaking the sound barrier, and more.
Author: James R. Hansen
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 990
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Book Description
Author: Eastman Nixon Jacobs
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 534
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Book Description
The results of tests of six airfoils having the N.A.C.A. 230 mean line and varying in thickness from 0.06c to 0.21c are presented. These results agree with previous findings in showing that aerodynamically the best section is one of moderate thickness. The data are of value mainly in connection with the design of tapered wings having sections based on the N.A.C.A. 230 mean line.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 764
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 516
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296
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Book Description
