Preliminary Investigation of the Effects of Several Seeker-nose Configurations on the Longitudinal Characteristics of a Canard-type Missile at a Mach Number of 1.60 PDF Download
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Author: A. Warner Robins
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32
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Book Description
Author: A. Warner Robins
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32
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Book Description
Author: A. Warner Robins
Publisher:
ISBN:
Category :
Languages : en
Pages : 25
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Book Description
Author: Robert C. Nelson
Publisher:
ISBN:
Category : History
Languages : en
Pages : 464
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Book Description
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author: Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 516
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Book Description
Author: Kenneth P. Werrell
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 308
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Book Description
Author: George M. Siouris
Publisher: Springer Science & Business Media
ISBN: 0387218165
Category : Technology & Engineering
Languages : en
Pages : 670
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Book Description
Airborne Vehicle Guidance and Control Systems is a broad and wide- angled engineering and technological area for research, and continues to be important not only in military defense systems but also in industrial process control and in commercial transportation networks such as various Global Positioning Systems (GPS). The book fills a long-standing gap in the literature. The author is retired from the Air Force Institute and received the Air Force's Outstanding Civilian Career Service Award.
Author: Denis Howe
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 488
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Book Description
Aircraft Conceptual Design Synthesis means design by fitness-for-purpose. Design engineers can jump off from the point of given parameters and requirements – required performance, payloads and other factors. This is the first book for the aeronautical designer devoted to guiding the reader through this highly effective conceptual design synthesis process. This forms the procedure for the initial stage of the aircraft design process – the interpretation of a requirement into the preliminary layout. A logical design sequence is developed utilizing original modules to represent propulsion, lift, drag, mass, and performance. Aircraft Conceptual Design Synthesis includes a disk of spreadsheets that provides core data. Unlike existing approaches, the design synthesis method can be applied to novel aircraft concepts. CONTENTS INCLUDE The design process Aircraft configuration Flight regime and powerplant considerations Fuselage layout Configuration of the wing Basic lift, drag and mass representations Performance estimation Parametric analysis and optimisation Analysis of concept design “This is an important landmark book and in my view will become a standard by which others will be compared” – Dr E C P Ransom, Kingston University, UK
Author: Albert C. Piccirillo
Publisher:
ISBN: 9781626830226
Category : Airplanes, Military
Languages : en
Pages : 328
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Book Description
Author: Jacob Neufeld
Publisher: DIANE Publishing
ISBN: 1437912877
Category : Technology & Engineering
Languages : en
Pages : 344
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Book Description
Proceedings of a symposium co-sponsored by the Air Force Historical Foundation and the Air Force History and Museums Program. The symposium covered relevant Air Force technologies ranging from the turbo-jet revolution of the 1930s to the stealth revolution of the 1990s. Illustrations.
Author: Thomas A. Keaney
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 296
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Book Description
