Missile Aerodynamics


Missile Aerodynamics
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Missile Aerodynamics


Missile Aerodynamics
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Author :
language : en
Publisher:
Release Date : 1974

Missile Aerodynamics written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics categories.




Missile Aerodynamics


Missile Aerodynamics
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Author : Jack N. Nielsen
language : en
Publisher:
Release Date : 1985

Missile Aerodynamics written by Jack N. Nielsen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985 with Guided missiles categories.




Missile Aerodynamics


Missile Aerodynamics
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Author : M. R. Mendenhall
language : en
Publisher:
Release Date : 1989-01-01

Missile Aerodynamics written by M. R. Mendenhall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989-01-01 with History categories.




Tactical Missile Aerodynamics General Topics


Tactical Missile Aerodynamics General Topics
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Author : M. R. Mendenhall
language : en
Publisher:
Release Date : 1992

Tactical Missile Aerodynamics General Topics written by M. R. Mendenhall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Guided missiles categories.




Missile Aerodynamics


Missile Aerodynamics
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Author : J. N. Nielsen
language : en
Publisher:
Release Date : 1960

Missile Aerodynamics written by J. N. Nielsen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.




Engineering Design Handbook


Engineering Design Handbook
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Author : United States. Army Materiel Command
language : en
Publisher:
Release Date : 1965

Engineering Design Handbook written by United States. Army Materiel Command and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aerodynamics categories.




Tactical Missile Aerodynamics


Tactical Missile Aerodynamics
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Author : M. R. Mendenhall
language : en
Publisher:
Release Date : 1992

Tactical Missile Aerodynamics written by M. R. Mendenhall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Guided missiles categories.




Aerodynamics Of Missiles And Rockets


Aerodynamics Of Missiles And Rockets
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Author : Mark Pinney
language : en
Publisher: McGraw-Hill Professional
Release Date : 2013-12-29

Aerodynamics Of Missiles And Rockets written by Mark Pinney and has been published by McGraw-Hill Professional this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-12-29 with Technology & Engineering categories.


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



Report


Report
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Author :
language : en
Publisher:
Release Date : 1965

Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Aeronautics categories.




Numerical Investigation Of Aerodynamics Of Canard Controlled Missile Using Planar And Grid Tail Fins


Numerical Investigation Of Aerodynamics Of Canard Controlled Missile Using Planar And Grid Tail Fins
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Author : James DeSpirito
language : en
Publisher:
Release Date : 2004

Numerical Investigation Of Aerodynamics Of Canard Controlled Missile Using Planar And Grid Tail Fins written by James DeSpirito and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2004 with Computational fluid dynamics categories.


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.