Body Surface Pressure Data On Two Monoplane Wing Missile Configurations With Elliptical Cross Sections At Mach 2 50

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Body Surface Pressure Data On Two Monoplane Wing Missile Configurations With Elliptical Cross Sections At Mach 2 50

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Author : Jerry M. Allen
language : en
Publisher:
Release Date : 1983

Body Surface Pressure Data On Two Monoplane Wing Missile Configurations With Elliptical Cross Sections At Mach 2 50 written by Jerry M. Allen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with Guided missiles categories.

Government Reports Announcements Index

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Author :
language : en
Publisher:
Release Date : 1984-02

Government Reports Announcements 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 1984-02 with Science categories.

Government Reports Annual Index

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Author :
language : en
Publisher:
Release Date : 1984

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 1984 with Government reports announcements & index categories.

Body Surface Pressure Data On Two Monoplane Wing Missile Configurations With Elliptical Cross Sections At Mach 2 50

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Author : Jerry M. Allen
language : en
Publisher:
Release Date : 1983

Body Surface Pressure Data On Two Monoplane Wing Missile Configurations With Elliptical Cross Sections At Mach 2 50 written by Jerry M. Allen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with Guided missiles categories.

An Improved Semiempirical Method For Calculating Aerodynamics Of Missiles With Noncircular Bodies

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Author : Frankie Gale Moore
language : en
Publisher:
Release Date : 1997

An Improved Semiempirical Method For Calculating Aerodynamics Of Missiles With Noncircular Bodies written by Frankie Gale Moore and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Aerodynamics categories.

Effect Of Nose Bluntness And Afterbody Shape On Aerodynamic Characteristics Of A Monoplanar Missile Concept With Bodies Of Circular And Elliptical Cross Sections At A Mach Number Of 2 50

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Author : Ernald B. Graves
language : en
Publisher:
Release Date : 1979

Effect Of Nose Bluntness And Afterbody Shape On Aerodynamic Characteristics Of A Monoplanar Missile Concept With Bodies Of Circular And Elliptical Cross Sections At A Mach Number Of 2 50 written by Ernald B. Graves and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aerodynamics categories.

Application Of Computational Fluid Dynamics To A Monoplane Fixed Wing Missile With Elliptic Cross Sections

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Author : Karen R. Heavey
language : en
Publisher:
Release Date : 2005

Application Of Computational Fluid Dynamics To A Monoplane Fixed Wing Missile With Elliptic Cross Sections written by Karen R. Heavey 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.

This report describes a computational study undertaken to investigate the performance of the CFD++ flow solver for prediction of nonlinear aerodynamics of a complex finned missile using structured hexahedral and unstructured tetrahedral grids. A monoplane fixed-wing missile with elliptic cross sections provided a geometrically complex model. Numerical solutions were obtained for this configuration at supersonic speed for various roll orientations, angles of attack, and jaw angles. Steady-state solutions were obtained using a three-dimensional Reynolds-Averaged Navier-Stokes solver with a two-equation turbulence model. Numerical results show the qualitative features of the flow fields at various cross-sectional and streamwise positions along the computational model of the missile. Aerodynamic coefficients were extracted from the computed solutions and found to match well with the available experimental data for these configurations. These numerical results show the effectiveness of using computational fluid dynamics techniques to produce an accurate prediction of the aerodynamics of geometrically complete configurations.

Effect Of Forebody Wing Strakes On Enhancing Performance Of A Typical Body Wing Tail Missile Configuration At Mach 2 0

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Author : Pamela K. Alstott
language : en
Publisher:
Release Date : 1980

Effect Of Forebody Wing Strakes On Enhancing Performance Of A Typical Body Wing Tail Missile Configuration At Mach 2 0 written by Pamela K. Alstott and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aerodynamics, Supersonic categories.

The addition of forebody strakes to aircraft configurations have shown significant improvement in aircraft performance at moderate-to-high angles-of-attack for subsonic nd transonic speeds. This research project investigates the effect of strakes on missile type body-wing-tail configurations at supersonic speeds by conducting a (1) literature survey of related existing data and design methods and (2) analyzing a new set of wind tunnel data on a body-wing-tail missile configuration with added forebody strakes at Mach 2.0. Findings from the literature survey are presented. Analysis of the wind tunnel data reveals that added forebody strakes do not significantly improve missile performance at Mach 2.0 and angles-of-attack up to 20 degrees for the configuration tested. (Author).

Improvements To The Missile Aerodynamic Prediction Code Demon3

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Author : National Aeronautics and Space Adm Nasa
language : en
Publisher: Independently Published
Release Date : 2018-11-22

Improvements To The Missile Aerodynamic Prediction Code Demon3 written by National Aeronautics and Space Adm Nasa and has been published by Independently Published this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-11-22 with Science categories.

The computer program DEMON3 was developed for the aerodynamic analysis of nonconventional supersonic configurations comprising a body with noncircular cross section and up to two wing or fin sections. Within a wing or fin section, the lifting surfaces may be cruciform, triform, planar, or low profile layouts; the planforms of the lifting surfaces allow for breaks in sweep. The body and fin sections are modeled by triplet and constant u-velocity panels, respectively, accounting for mutual body-fin interference. Fin thickness effects are included for the use of supersonic planar source panels. One of the unique features of DEMON3 is the modeling of high angle of attack vortical effects associated with the lifting surfaces and the body. In addition, shock expansion and Newtonian pressure calculation methods can be optionally engaged. These two dimensional nonlinear methods are augmented by aerodynamic interference determined from the linear panel methods. Depending on the geometric details of the body, the DEMON3 program can be used to analyze nonconventional configurations at angles of attack up to 25 degrees for Mach numbers from 1.1 to 6. Calculative results and comparisons with experimental data demonstrate the capabilities of DEMON3. Limitations and deficiencies are listed. Dillenius, Marnix F. E. and Johnson, David L. and Lesieutre, Daniel J. AERODYNAMIC CHARACTERISTICS; AERODYNAMICS; BODY-WING AND TAIL CONFIGURATIONS; COMPUTER PROGRAMS; DESIGN ANALYSIS; FINS; MISSILE DESIGN; MISSILES; PANEL METHOD (FLUID DYNAMICS); WINGS; AERODYNAMIC INTERFERENCE; ANGLE OF ATTACK; LAYOUTS; NEWTON METHODS; NONLINEARITY; PLANFORMS; THICKNESS; TRANSONIC SPEED...

Application Of Computational Fluid Dynamics To A Monoplane Fixed Wing Missile With Elliptic Cross Sections

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Author : Karen R. Heavey
language : en
Publisher:
Release Date : 2005

Application Of Computational Fluid Dynamics To A Monoplane Fixed Wing Missile With Elliptic Cross Sections written by Karen R. Heavey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with Fluid dynamics categories.