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Aerodynamic Configured Missile Development
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Book Synopsis Aerodynamic Configured Missile Development by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development written by Robert J. Krieger and published by . This book was released on 1980 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Aerodynamic Configured Missile Development by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development written by Robert J. Krieger and published by . This book was released on 1980 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Aerodynamic Configured Missile Development by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development written by Robert J. Krieger and published by . This book was released on 1980 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Aerodynamic Configured Missile Development by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development written by Robert J. Krieger and published by . This book was released on 1980 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Aerodynamic Configured Missile Development by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development written by Robert J. Krieger and published by . This book was released on 1980 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Missile Configuration Design by : S. S. Chin
Download or read book Missile Configuration Design written by S. S. Chin and published by . This book was released on 1961 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt: Beskriver principperne i f.m. konstruktionen af styrede missiler.
Book Synopsis Aerodynamic Configured Missile Development by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development written by Robert J. Krieger and published by . This book was released on 1980 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Aerodynamic Configured Missile Development Final Report by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development Final Report written by Robert J. Krieger and published by . This book was released on 1980 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Test and Analysis of a Slender Generic Missile Configuration by : Roger S. Gates
Download or read book Aerodynamic Test and Analysis of a Slender Generic Missile Configuration written by Roger S. Gates and published by . This book was released on 1989 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Engineering Design Handbook by : United States. Army Materiel Command
Download or read book Engineering Design Handbook written by United States. Army Materiel Command and published by . This book was released on 1965 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Stability Technology for Maneuverable Missiles by : Gennaro F. Aiello
Download or read book Aerodynamic Stability Technology for Maneuverable Missiles written by Gennaro F. Aiello and published by . This book was released on 1979 with total page 396 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study developed empirical methods to predict aerodynamic characteristics of body-tail, body-wing-tail and body-strake-tail missile configurations. Methods cover the Mach number range from 0.6 to 3.0. Methods cover the individual body and tail characteristics at angles of attack from 0 to 180 degrees. For winged bodies the methods encompass angles of attack up to about 30 degrees. All mutual interference effects are accounted for, allowing accurate prediction of force and moment coefficients. (Author).
Book Synopsis Studies on Dynamics and Instrumentation of the Holloman Track by : Air Force Missile Development Center (U.S.)
Download or read book Studies on Dynamics and Instrumentation of the Holloman Track written by Air Force Missile Development Center (U.S.) and published by . This book was released on 1959 with total page 634 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Eugene L. Fleeman Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :530 pages Book Rating :4.F/5 ( download)
Book Synopsis Tactical Missile Design by : Eugene L. Fleeman
Download or read book Tactical Missile Design written by Eugene L. Fleeman and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2006 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt: This textbook will provide a basis for including tactical missile design as part of the aerospace engineering curriculum, providing new graduates with the knowledge they will need in their careers.
Author :Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial Publisher : ISBN 13 :9789283504528 Total Pages :758 pages Book Rating :4.5/5 (45 download)
Book Synopsis Special Course on Missile Aerodynamics by : Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial
Download or read book Special Course on Missile Aerodynamics written by Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial and published by . This book was released on 1988 with total page 758 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Missile Aerodynamics written by and published by . This book was released on 1974 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Next Generation Missile Design by : J. E. Williams
Download or read book Next Generation Missile Design written by J. E. Williams and published by . This book was released on 1988 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt: To meet operational requirements, the next generation of long range cruise class missiles will fly at relatively high altitudes and supersonic or hypersonic speeds. Low cost design and development approaches must be used. To illustrate these approaches, the results of the USAF sponsored Aerodynamic Configured Missile (ACM) Program and the subsequent Low Cost Aerodynamic Configured Missile Demonstrator Program are summarized with emphasis on the impact of these studies on future missile concepts. The ACM program objective was to exploit the aerodynamic potential of supersonic cruise and maneuvering missiles to achieve significant improvements in performance. Configuration development, wind tunnel testing, and performance analyses were performed. Major uses of the program results to date are described. These uses include points of departure concepts, prediction models, evaluation of prediction models, and evaluation of other missile concepts. A low cost flight program plan is described with the goal to demonstrate missile flight at high supersonic Mach numbers with high lift-to-drag ratios. A low cost approach is described which uses existing equipment, standard airframe structural design, the existing ACM data base, trajectory shaping and aggressive program planning. Two flight test options identified are wing-body concept. The design described is an ACM airframe which provides a test bed for a variety of experiments.
Book Synopsis An Aerodynamic Assessment of Various Missile Configuration Concepts by :
Download or read book An Aerodynamic Assessment of Various Missile Configuration Concepts written by and published by . This book was released on 1983 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
