Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds
Author: A. J. Eggers
Publisher:
Published: 1950
Total Pages: 262
ISBN-13:
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Author: A. J. Eggers
Publisher:
Published: 1950
Total Pages: 262
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1950
Total Pages: 996
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1955
Total Pages:
ISBN-13:
DOWNLOAD EBOOKIncludes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: G. N. Ward
Publisher: Cambridge University Press
Published: 2016-02-25
Total Pages: 261
ISBN-13: 1316601897
DOWNLOAD EBOOKOriginally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Author:
Publisher:
Published: 1951
Total Pages: 234
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1954
Total Pages: 1078
ISBN-13:
DOWNLOAD EBOOKAuthor: Elmer A. Horton
Publisher:
Published: 1950
Total Pages: 678
ISBN-13:
DOWNLOAD EBOOKAn investigation was made to determine the effects of boundary-layer control on the landing performance characteristics of a liaison type of airplane having a payload of 1500 pounds and a flight duration of 5 hours. The aspect ratio was varied from 5 to 15, the wing span from 30 to 100 feet, and the brake horsepower from 300 to 1200. The use of boundary-layer control caused reduction in total landing distance (25 to 40 percent), ground-run distance, gliding speed, and stalling speed whereas sinking speed was increased only slightly.
Author: Holt Ashley
Publisher: Courier Corporation
Published: 2013-05-27
Total Pages: 402
ISBN-13: 0486166538
DOWNLOAD EBOOK"Written by one of the leading aerospace educators of our time, each sentence is packed with information. An outstanding book." — Private Pilot "Illuminated throughout by new twists in explaining familiar concepts, helpful examples and intriguing ‘by-the-ways.’ A fine book." — Canadian Aeronautics and Space Journal This classic by a Stanford University educator and a pioneer of aerospace engineering introduces the complex process of designing atmospheric flight vehicles. An exploration of virtually every important subject in the fields of subsonic, transonic, supersonic, and hypersonic aerodynamics and dynamics, the text demonstrates how these topics interface and how they complement one another in atmospheric flight vehicle design. The mathematically rigorous treatment is geared toward graduate-level students, and it also serves as an excellent reference. Problems at the end of each chapter encourage further investigation of the text’s material, the study of fresh ideas, and the exploration of new areas.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1955
Total Pages: 38
ISBN-13:
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