Aerodynamic Configured Missile Development Final Report PDF Download
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Author: Robert J. Krieger
Publisher:
ISBN:
Category : Cruise missiles
Languages : en
Pages : 580
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Book Description
Author: Robert J. Krieger
Publisher:
ISBN:
Category : Cruise missiles
Languages : en
Pages : 580
Get Book Here
Book Description
Author: Robert J. Krieger
Publisher:
ISBN:
Category : Cruise missiles
Languages : en
Pages : 86
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Book Description
This report presents the results of a program that investigated aerodynamic configuring as a method of improving long range supersonic cruise and maneuvering missile performance. Non-circular body, lifting body, blended wing body, wing-body and favorable interference concepts were developed and wind tunnel tested. Substantial improvements in cruise range were shown to result from aero configuring.
Author: Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial
Publisher:
ISBN: 9789283504528
Category : Guided missiles
Languages : en
Pages : 758
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Book Description
Author: Jack Norman Nielsen
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9780962062902
Category : Guided missiles
Languages : en
Pages : 450
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Book Description
The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. " Missile Aerodynamics," a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.
Author: Eugene L. Fleeman
Publisher: AIAA Education
ISBN: 9781600869082
Category : Technology & Engineering
Languages : en
Pages : 0
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Book Description
"In his latest book, Missile Design and System Engineering, Eugene L. Fleeman comprehensively reviews the missile design and system engineering process, drawing on his decades of experience in designing and developing missile systems. Addressing the needs of aerospace engineering students and professors, systems analysts and engineers, and program managers, the book examines missile design, missile technologies, launch platform integration, missile system measures of merit, and the missile system development process. This book has been adapted from Fleeman's earlier title, Tactical Missile Design, Second Edition, to include a greater emphasis on system engineering." --Back cover.
Author: Robert J. Krieger
Publisher:
ISBN:
Category : Cruise missiles
Languages : en
Pages : 76
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Book Description
This report presents the results of a program that investigated aerodynamic configuring as a method of improving long range supersonic cruise and maneuvering missile performance. Non-circular body, lifting body, blended wing body, wing-body and favorable interference concepts were developed and wind tunnel tested. Substantial improvements in cruise range were shown to result from aero configuring.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 636
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 866
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Book Description
Author: Robert J. Krieger
Publisher:
ISBN:
Category : Cruise missiles
Languages : en
Pages : 136
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Book Description
This report presents the results of a program that investigated aerodynamic configuring as a method of improving long range supersonic cruise and maneuvering missile performance. Non-circular body, lifting body, blended wing body, wing-body and favorable interference concepts were developed and wind tunnel tested. Substantial improvements in cruise range were shown to result from aero configuring.
