Missile Aerodynamics

Author : Jack Norman Nielsen
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 450 pages
File Size : 55,7 Mb
Release : 1988-01-01
Category : Guided missiles
ISBN : 0962062901

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Missile Aerodynamics by Jack Norman Nielsen Pdf

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 : Anonim
Publisher : Unknown
Page : 356 pages
File Size : 43,5 Mb
Release : 1974
Category : Aerodynamics
ISBN : PSU:000017295017

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Missile Aerodynamics by Anonim Pdf

Author : M. R. Mendenhall,David Nixon,Marnix F. E. Dillenius
Publisher : Unknown
Page : 128 pages
File Size : 52,9 Mb
Release : 1989-01-01
Category : History
ISBN : 096206291X

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Missile Aerodynamics by M. R. Mendenhall,David Nixon,Marnix F. E. Dillenius Pdf

Author : Frankie Gale Moore,Roy Mitchell McInville,Tom Hymer
Publisher : Unknown
Page : 148 pages
File Size : 42,8 Mb
Release : 1997
Category : Aerodynamics
ISBN : UOM:39015095342120

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An Improved Semiempirical Method for Calculating Aerodynamics of Missiles with Noncircular Bodies by Frankie Gale Moore,Roy Mitchell McInville,Tom Hymer Pdf

Author : United States. Army Materiel Command
Publisher : Unknown
Page : 108 pages
File Size : 49,5 Mb
Release : 1965
Category : Aerodynamics
ISBN : MINN:31951T00411573P

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Engineering Design Handbook by United States. Army Materiel Command Pdf

Author : Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial. Consultant and Exchange Programme
Publisher : Unknown
Page : 758 pages
File Size : 52,5 Mb
Release : 1988
Category : Guided missiles
ISBN : 9283504526

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Special Course on Missile Aerodynamics by Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial. Consultant and Exchange Programme Pdf

Author : M. R. Mendenhall
Publisher : Unknown
Page : 774 pages
File Size : 46,9 Mb
Release : 1992
Category : Guided missiles
ISBN : UOM:39015021574630

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Tactical Missile Aerodynamics: General topics by M. R. Mendenhall Pdf

Author : American Institute of Aeronautics and Astronautics
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
Page : 806 pages
File Size : 48,7 Mb
Release : 1992
Category : Guided missiles
ISBN : 1563470160

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Tactical Missile Aerodynamics by American Institute of Aeronautics and Astronautics Pdf

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 : J. N. Nielsen
Publisher : Unknown
Page : 128 pages
File Size : 52,5 Mb
Release : 1960
Category : Electronic
ISBN : OCLC:500206748

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Missile Aerodynamics by J. N. Nielsen Pdf

Author : James DeSpirito,Vaughn, Milton E.,Washington, W. David
Publisher : Unknown
Page : 212 pages
File Size : 50,7 Mb
Release : 2004
Category : Computational fluid dynamics
ISBN : UOM:39015095299676

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Numerical Investigation of Aerodynamics of Canard-controlled Missile Using Planar and Grid Tail Fins by James DeSpirito,Vaughn, Milton E.,Washington, W. David Pdf

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.

Author : Eugene L. Fleeman,Joseph A. Schetz
Publisher : AIAA Education
Page : 0 pages
File Size : 40,9 Mb
Release : 2012
Category : Technology & Engineering
ISBN : 1600869084

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Missile Design and System Engineering by Eugene L. Fleeman,Joseph A. Schetz Pdf

"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 : Anonim
Publisher : Unknown
Page : 282 pages
File Size : 53,8 Mb
Release : 1974
Category : Aerodynamics
ISBN : PSU:000018994025

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Missile Aerodynamics by Anonim Pdf

Author : Anonim
Publisher : Unknown
Page : 440 pages
File Size : 50,7 Mb
Release : 1995
Category : Aeronautics
ISBN : MINN:30000006324267

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Scientific and Technical Aerospace Reports by Anonim Pdf

Author : Michael J. Hemsch,Jack Norman Nielsen
Publisher : Unknown
Page : 890 pages
File Size : 44,7 Mb
Release : 1986
Category : Technology & Engineering
ISBN : UOM:39015011191429

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Tactical Missile Aerodynamics by Michael J. Hemsch,Jack Norman Nielsen Pdf

Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
Page : 38 pages
File Size : 43,8 Mb
Release : 2018-10-15
Category : Science
ISBN : 1728741173

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The Present Status and the Future of Missile Aerodynamics by National Aeronautics and Space Adm Nasa Pdf

Some recent developments in the state of the art in missile aerodynamics are reviewed. Among the subjects covered are: (1) tri-service/NASA data base, (2) wing-body interference, (3) nonlinear controls, (4) hypersonic transition, (5) vortex interference, (6) airbreathers, supersonic inlets, (7) store separation problems, (8) correlation of missile data, (9) CFD codes for complete configurations, (10) engineering prediction methods, and (11) future configurations. Suggestions are made for future research and development to advance the state of the art of missile aerodynamics. Nielsen, Jack N. Ames Research Center