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Missile Aerodynamics
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Author :Jack Norman Nielsen Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 :9780962062902 Total Pages :450 pages Book Rating :4.0/5 (629 download)
Book Synopsis Missile Aerodynamics by : Jack Norman Nielsen
Download or read book Missile Aerodynamics written by Jack Norman Nielsen and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1988-01-01 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
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:
Download or read book Missile Aerodynamics written by and published by . This book was released on 1974 with total page 282 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tactical Missile Aerodynamics by : Michael J. Hemsch
Download or read book Tactical Missile Aerodynamics written by Michael J. Hemsch and published by . This book was released on 1986 with total page 890 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 Missile Aerodynamics by : M. R. Mendenhall
Download or read book Missile Aerodynamics written by M. R. Mendenhall and published by . This book was released on 1989-01-01 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tactical Missile Aerodynamics by : M. R. Mendenhall
Download or read book Tactical Missile Aerodynamics written by M. R. Mendenhall and published by . This book was released on 1992 with total page 806 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Numerical Investigation of Aerodynamics of Canard-controlled Missile Using Planar and Grid Tail Fins by : James DeSpirito
Download or read book Numerical Investigation of Aerodynamics of Canard-controlled Missile Using Planar and Grid Tail Fins written by James DeSpirito and published by . This book was released on 2004 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt: Viscous computational fluid dynamic simulations were used to predict the aerodynamic coefficients and flow field around a canard-controlled missile in subsonic and transonic flow. Computations were performed at Mach 0.6 and 0.9, six angles of attack between 0 deg and 10 deg, and with planar and grid tail fins. The computations were validated with wind tunnel data. Flow visualizations showed that the canard downwash produced a low-pressure region on the starboard side of the missile that produced a large induced side force. The canard trailing vortices interacted with the tail fins until alpha> 8 deg, producing a pressure differential on the leeward tail fin, leading to the adverse induced roll effects. Visualizations of the flow through the grid fin structure showed choking of the flow at Mach 0.9 and Mach 1.5. The validated simulations results showed that grid fins did not improve the canard roll-control effectiveness at subsonic and transonic speeds as well as they did at the low supersonic speed.
Download or read book Tactical Missile Aerodynamics written by and published by . This book was released on 1992 with total page 731 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tactical Missile Aerodynamics: General topics by : M. R. Mendenhall
Download or read book Tactical Missile Aerodynamics: General topics written by M. R. Mendenhall and published by . This book was released on 1992 with total page 774 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Present Status and the Future of Missile Aerodynamics by :
Download or read book The Present Status and the Future of Missile Aerodynamics written by and published by . This book was released on 1988 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Missile Design and System Engineering by : Eugene L. Fleeman
Download or read book Missile Design and System Engineering written by Eugene L. Fleeman and published by AIAA Education. This book was released on 2012 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: "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 :American Institute of Aeronautics and Astronautics Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 :9781563470165 Total Pages :806 pages Book Rating :4.4/5 (71 download)
Book Synopsis Tactical Missile Aerodynamics by : American Institute of Aeronautics and Astronautics
Download or read book Tactical Missile Aerodynamics written by American Institute of Aeronautics and Astronautics and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1992 with total page 806 pages. Available in PDF, EPUB and Kindle. Book excerpt: Prediction Methodology contains updated versions of nine chapters from the first edition and chapters on drag prediction, component build-up methods, Euler methods and Navier-Stokes solvers. Special attention is paid to nonlinear flow phenomena and unconventional airframe shapes. Eight colour plates and more than 540 figures are included.
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:
Book Synopsis Missile Aerodynamics by : J. N. Nielsen
Download or read book Missile Aerodynamics written by J. N. Nielsen and published by . This book was released on 1960 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamics of Missiles and Rockets by : Mark Pinney
Download or read book Aerodynamics of Missiles and Rockets written by Mark Pinney and published by McGraw-Hill Professional. This book was released on 2013-12-29 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Proven techniques for deriving the basic aerodynamic properties of axisymmetric-shaped bodies with the minimum amount of time and effort Aerodynamics of Missiles and Rockets describes the basic aerodynamics model used in the widespread Analytical Initial Missile Synthesis (AIMS) computer code for symmetric missile and rocket sizing and design. It is a collection of empirical, semi-empirical and theoretical aerodynamics engineering methods for a component build-up approach to aerodynamics prediction. This book serves as an on-the-job application manual and desk reference for the prediction of basic aerodynamics. It can also be used for courses in applied aerodynamics in Mechanical and Aerospace Engineering programs and for short courses in industry and government. This practical guide provides an alternative approach to utilizing numerous, complex, stand-alone computer codes, but is also a good complement to these codes. The book offers insight into the methods and techniques used to derive answers and correct magnitudes generated by code, giving confidence in final results. Features a Microsoft Excel file that automates calculations and provides complete tabulated output for missile and rocket geometry and design, and design and for rapid assessments of aerodynamic properties based on changes in geometry or flight conditions On-the-job application manual and desk reference for the prediction of basic aerodynamics Combination of long-standing, empirical and semi-empirical techniques with classical aerodynamic theory A component build-up approach utilized, with body and wing/tail surface aerodynamics determined separately and then combined for total configuration zero-lift drag, lift, center of pressure location, and pitching moment
