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Base Pressure Computations Of The Dera Generic Missile Wind Tunnel Model


Base Pressure Computations Of The Dera Generic Missile Wind Tunnel Model
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Base Pressure Computations Of The Dera Generic Missile Wind Tunnel Model


Base Pressure Computations Of The Dera Generic Missile Wind Tunnel Model
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Author : James DeSpirito
language : en
Publisher:
Release Date : 2005

Base Pressure Computations Of The Dera Generic Missile Wind Tunnel Model 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 2005 with Computational fluid dynamics categories.


Computational fluid dynamic simulations were used to compute the aerodynamic coefficients of a body-alone missile and a planar fin missile in the presence of a wind tunnel sting. The investigation was an extension to a previous investigation in which the computed forebody axial force did not compare well with experimental wind tunnel data, while all other forces and moments showed excellent agreement. The current investigation showed that the computed results are accurate, predicting the total axial force to within 5% of the experimental values. The results indicate that the discrepancy in the forebody axial force is due to an inaccurate experimental base pressure measurement.



Base Pressure Computations Of The Dera Generic Missile Wind Tunnel Model


Base Pressure Computations Of The Dera Generic Missile Wind Tunnel Model
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 2005

Base Pressure Computations Of The Dera Generic Missile Wind Tunnel Model written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with categories.


Computational fluid dynamic simulations were used to compute the aerodynamic coefficients of a body-alone missile and a planar fin missile in the presence of a wind tunnel sting. The investigation was an extension to a previous investigation in which the computed forebody axial force did not compare well with experimental wind tunnel data, while all other forces and moments showed excellent agreement. The current investigation showed that the computed results are accurate, predicting the total axial force to within 5% of the experimental values. The results indicate that the discrepancy in the forebody axial force is due to an inaccurate experimental base pressure measurement.



Computational Fluid Dynamic Cfd Analysis Of A Generic Missile With Grid Fins


Computational Fluid Dynamic Cfd Analysis Of A Generic Missile With Grid Fins
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Author : James DeSpirito
language : en
Publisher:
Release Date : 2000

Computational Fluid Dynamic Cfd Analysis Of A Generic Missile With Grid 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 2000 with Computational fluid dynamics categories.


This report presents the results of a study demonstrating an approach for using viscous computational fluid dynamic simulations to calculate the flow field and aerodynamic coefficients for a missile with grid fin. A grid fin is an unconventional lifting and control surface that consists of an outer frame supporting an inner grid of intersecting planar surfaces of small chord. The calculations were made at a Mach number of 2.5 and several angles of attack for a missile without fins, with planar fms, and with grid fins. The results were validated by comparing the computed aerodynamic coefficients for the missile and individual grid fins against wind tunnel measurement data. Very good agreement with the measured data was observed for all configurations investigated. For the grid fin case, the aerodynamic coefficients were within 2.8-6.5% of the wind tunnel data. The normal force coefficients on the individual grid fins were within 11% of the test data. The simulations were also successful in calculating the flow structure around the fin in the separated-flow region at the higher angles of attack. This was evident in the successful calculation of the nonlinear behavior for that fin, which showed negative normal force at the higher angles of attack. The effective angle of attack is negative on either part of or all of the top grid fin for the higher angles of attack.



International Aerospace Abstracts


International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1999

International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Aeronautics categories.




High Speed Wind Tunnels


High Speed Wind Tunnels
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Author : Luigi Crocco
language : en
Publisher:
Release Date : 1946

High Speed Wind Tunnels written by Luigi Crocco and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1946 with Aerodynamics, Supersonic categories.


The importance assumed in recent times by experimental supersonic wind tunnels, as well as the power required, has brought about the need for a study which would permit a comparison of the types tested and the principal theoretical plans.



Modern Engineering For Design Of Liquid Propellant Rocket Engines


Modern Engineering For Design Of Liquid Propellant Rocket Engines
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Author : Dieter K. Huzel
language : en
Publisher: AIAA
Release Date : 1992

Modern Engineering For Design Of Liquid Propellant Rocket Engines written by Dieter K. Huzel and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Liquid propellant rocket engines categories.




Pressure And Temperature Sensitive Paints


Pressure And Temperature Sensitive Paints
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Author : Tianshu Liu
language : en
Publisher: Springer Science & Business Media
Release Date : 2005

Pressure And Temperature Sensitive Paints written by Tianshu Liu and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with Science categories.


Luminescent molecule sensors, called pressure-sensitive paint (PSP) and temperature-sensitive paint (TSP), measure factors essential for understanding the aerodynamic performance and heat transfer characteristics of flight vehicles. They provide a powerful tool for experimental aerodynamicists to obtain a deeper understanding of the rich physical phenomena in complex flows around a flight vehicle. This book helps the reader to understand the physics and chemistry and the capabilities of PSP and TSP. It provides an overview of the wide scope of applications and explains the system requirements for using these sensors. The book also includes an extensive table of properties of PTP and TSP. As such, it is a thorough and up-to-date coverage of the underlying physics and applications of luminescent molecules designed for global pressure and temperature mapping



Engineering Mechanics Of Composite Materials


Engineering Mechanics Of Composite Materials
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Author : Isaac M. Daniel
language : en
Publisher: Oxford University Press, USA
Release Date : 2006

Engineering Mechanics Of Composite Materials written by Isaac M. Daniel and has been published by Oxford University Press, USA this book supported file pdf, txt, epub, kindle and other format this book has been release on 2006 with Composite materials categories.


"Engineering Mechanics of Composite Materials, Second Edition, is ideal for advanced undergraduate and introductory graduate courses on composite materials in materials science and mechanical engineering."--BOOK JACKET.



Wind Tunnel Wall Correction


Wind Tunnel Wall Correction
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Author : B. F. R. Ewald
language : en
Publisher:
Release Date : 1998

Wind Tunnel Wall Correction written by B. F. R. Ewald and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aerodynamics categories.


This report was compiled by an international team of wind tunnel wall correction experts. It presents the present state of the art in wind tunnel wall corrections with a special emphasis given to the description of modern wall correction methods based on Computational Fluid Dynamics. This AGARDograph was planned by the AGARD Fluid Dynamics Panel to be a modern sequel of the successful AGARDograph 109 "Subsonic Wind Tunnel Wall Corrections", which was published in 1966. AGARDogaph 109 is still valid and continues to be used to provide wall corrections in many wind tunnels. Nevertheless, in the thirty two years since the publication of AGARDograph 109, much work has been done on the subject, and the influence of the new tool of numerical fluid dynamics was so strong, that a sequel to AGARDograph 109 was considered to be necessary.



Government Reports Annual Index


Government Reports Annual Index
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Author :
language : en
Publisher:
Release Date : 1994

Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Government reports announcements & index categories.