Improvements To The Missile Aerodynamic Prediction Code Demons
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Improvements To The Missile Aerodynamic Prediction Code Demons
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1992
Improvements To The Missile Aerodynamic Prediction Code Demons written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.
Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1995
Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Mechanics, Applied categories.
Special Course On Missile Aerodynamics
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Author : Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial
language : en
Publisher:
Release Date : 1988
Special Course On Missile Aerodynamics written by Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with Guided missiles categories.
Longitudinal Control And Footprint Analysis For A Reusable Military Launch Vehicle
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Author : Anhtuan D. Ngo
language : en
Publisher:
Release Date : 2003
Longitudinal Control And Footprint Analysis For A Reusable Military Launch Vehicle written by Anhtuan D. Ngo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2003 with Launch vehicles (Astronautics) categories.
In this paper, we will examine a configuration for a reusable military launch vehicle (RMLS) concept. This configuration allows for the vehicle to land in an inverted attitude. Such inverted landing improves the turnaround time of the vehicle by reducing the maintenance requirements of the vehicle's thermal protection system. An analysis is performed to examine the impacts by the configuration on stability, control, and footprint for an RMLS configuration.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1990
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 1990 with Science categories.
International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1989
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 1989 with Aeronautics categories.
Aeronautical Engineering
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Author :
language : en
Publisher:
Release Date : 1982
Aeronautical Engineering written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Aeronautics categories.
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Nasa Sp
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Author :
language : en
Publisher:
Release Date : 1982
Nasa Sp written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Aeronautics categories.
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...
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1982-10
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982-10 with Aeronautics categories.