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Missile Datcom Users Manual
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Book Synopsis Missile Datcom User's Manual by : William B. Blake
Download or read book Missile Datcom User's Manual written by William B. Blake and published by . This book was released on 1998 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report is a User's Manual for the 1997 FORTRAN 90 revision of the Missile Datcom computer program. This supersedes WL-TR-93-3043. In missile preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of missile configuration designs. Since the ultimate shape and aerodynamic performance are so dependent upon the subsystems utilized, such as payload size, propulsion system selection and launch mechanism, the designer must be capable of predicting a wide variety of configurations accurately. The fundamental purpose of Missile Datcom is to provide an aerodynamic design tool which has the predictive accuracy suitable for preliminary design, and the capability for the user to easily substitute methods to fit specific applications.
Download or read book Missile Datcom written by Kevin D. Bruns and published by . This book was released on 1991 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Missile Datcom by : William B. Blake
Download or read book Missile Datcom written by William B. Blake and published by . This book was released on 1998-02-01 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt: THIS REPORT IS A USER'S MANUAL FOR THE 1997 FORTRAN 90 REVISION OF THE MISSILE DATCOM COMPUTER PROGRAM. THIS SUPERSEDES WL-TR-93-3043. In missile preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of missile configuration designs. Since the ultimate shape and aerodynamic performance are so dependent upon the subsystems utilized, such as payload size, propulsion system selection and launch mechanism, the designer must be capable of predicting a wide variety of configurations accurately. The fundamental purpose of Missile Datcom is to provide an aerodynamic design tool which has the predictive accuracy suitable for preliminary design, and the capability for the user to easily substitute methods to fit specific applications.
Book Synopsis Missile Datcom, User's Manual by : Keith A. Burns
Download or read book Missile Datcom, User's Manual written by Keith A. Burns and published by . This book was released on 1993 with total page 226 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Missile Datcom, User's Manual -- Revision 6/93 by : Keith A. Burns
Download or read book Missile Datcom, User's Manual -- Revision 6/93 written by Keith A. Burns and published by . This book was released on 1993 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt: In missile preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of missile configuration designs. Since the ultimate shape and aerodynamic performance are so dependent upon the subsystems utilized, such as payload size, propulsion system selection and launch mechanism, the designer must be capable of predicting a wide variety of configurations accurately. The fundamental purpose of Missile Datcom is to provide an aerodynamic design tool which has the predictive accuracy suitable for preliminary design, and the capability for the user to easily substitute methods to fit specific applications.
Book Synopsis Missile Datcom. User's Manual - Rev 4/91 by : Kevin D. Bruns
Download or read book Missile Datcom. User's Manual - Rev 4/91 written by Kevin D. Bruns and published by . This book was released on 1991 with total page 129 pages. Available in PDF, EPUB and Kindle. Book excerpt: In missile preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of missile configuration designs. Since the ultimate shape and aerodynamic performance are so dependent upon the subsystems used, such as payload size, propulsion system selection and launch mechanism, the designer must be capable of predicting a wide variety of configurations accurately. The fundamental purpose of Missile Datcom is to provide an aerodynamic design tool which has the predictive accuracy suitable for preliminary design, and the capability for the user to easily substitute methods to fit specific applications.
Book Synopsis Missile Datcom by : Steven R. Vukelich
Download or read book Missile Datcom written by Steven R. Vukelich and published by . This book was released on 1988 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The computer code is capable of addressing a wide variety of conventional missile designs. For the purposes of this document, a conventional missile is one which is comprised of the following: An axisymmetric or elliptically-shaped body, One to four fin sets located along the body between the nose and base. Each fin set can be comprised of one to eight identical panels attached around the body at a common longitudinal position, and An airbreathing propulsion system. To minimize the quantity of input data required, commonly used values for many inputs are assumed as defaults. However, all program defaults can be over-ridden by the user in order to more accurately model the configuration of interest.
Book Synopsis Missile Datcom by : Steven R. Vukelich
Download or read book Missile Datcom written by Steven R. Vukelich and published by . This book was released on 1988 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt: The computer code is capable of addressing a wide variety of conventional missile designs. For the purposes of this document, a conventional missile is one which is comprised of the following: An axisymmetric or elliptically-shaped body, One to four fin sets located along the body between the nose and base. Each fin set can be comprised of one to eight identical panels attached around the body at a common longitudinal position, and An airbreathing propulsion system. To minimize the quantity of input data required, commonly used values for many inputs are assumed as defaults. However, all program defaults can be over-ridden by the user in order to more accurately model the configuration of interest.
Book Synopsis Missile Datcom by : Steven R. Vukelich
Download or read book Missile Datcom written by Steven R. Vukelich and published by . This book was released on 1988 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt: Development of a Missile DATCOM handbook and computer program is described. The type of methods investigated as well as a method selection rationale is discussed. Methods were selected for predicting the aerodynamics of missile configurations made up of circular, elliptic or arbitrary bodies with or without fins an inlets. These methods predict static and dynamic stability derivatives and are suitable for preliminary design. A summary of the comparisons of many results with experimental data is included. Keywords: Computer aided design, DATCOM computer program, FORTRAN, Subsonic, Transonic, Supersonic, Hypersonic.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 728 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle by : Anhtuan D. Ngo
Download or read book Longitudinal Control and Footprint Analysis for a Reusable Military Launch Vehicle written by Anhtuan D. Ngo and published by . This book was released on 2003 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Missile DATCOM written by and published by . This book was released on 1988 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt: Development of a Missile DATCOM handbook and computer program is described. The type of methods investigated as well as a method selection rationale is discussed. Methods were selected for predicting the aerodynamics of missile configurations made up of circular, elliptic or arbitrary bodies with or without fins an inlets. These methods predict static and dynamic stability derivatives and are suitable for preliminary design. A summary of the comparisons of many results with experimental data is included. Keywords: Computer aided design, DATCOM computer program, FORTRAN, Subsonic, Transonic, Supersonic, Hypersonic.
Book Synopsis Technical Reports Awareness Circular : TRAC. by :
Download or read book Technical Reports Awareness Circular : TRAC. written by and published by . This book was released on 1989-08 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Damien Tromeur-Dervout Publisher :Springer Science & Business Media ISBN 13 :3642144381 Total Pages :428 pages Book Rating :4.6/5 (421 download)
Book Synopsis Parallel Computational Fluid Dynamics 2008 by : Damien Tromeur-Dervout
Download or read book Parallel Computational Fluid Dynamics 2008 written by Damien Tromeur-Dervout and published by Springer Science & Business Media. This book was released on 2010-09-21 with total page 428 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book collects the proceedings of the Parallel Computational Fluid Dynamics 2008 conference held in Lyon, France. Contributed papers by over 40 researchers representing the state of the art in parallel CFD and architecture from Asia, Europe, and North America examine major developments in (1) block-structured grid and boundary methods to simulate flows over moving bodies, (2) specific methods for optimization in Aerodynamics Design, (3) innovative parallel algorithms and numerical solvers, such as scalable algebraic multilevel preconditioners and the acceleration of iterative solutions, (4) software frameworks and component architectures for parallelism, (5) large scale computing and parallel efficiencies in the industrial context, (6) lattice Boltzmann and SPH methods, and (7) applications in the environment, biofluids, and nuclear engineering.
Book Synopsis Advanced Aircraft Flight Performance by : Antonio Filippone
Download or read book Advanced Aircraft Flight Performance written by Antonio Filippone and published by Cambridge University Press. This book was released on 2012-12-17 with total page 665 pages. Available in PDF, EPUB and Kindle. Book excerpt: This unique book deals with the aeroplane at several levels and aims to simulate its flight performance using computer software.
Book Synopsis Development Feasibility of Missile Datcom by : Steven R. Vukelich
Download or read book Development Feasibility of Missile Datcom written by Steven R. Vukelich and published by . This book was released on 1981 with total page 310 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report summarizes the methods available to predict the aerodynamic static, dynamic, and control characteristics of missiles. The methods selected for Missile Datcom development were based upon a criteria which included ease of use, accuracy, utility over a range of flight conditions and cost effective in their use. This report describes the methodology appropriate for the missile designer. An outline of a Missile Datcom handbook is proposed; an automated version is also recommended for development. Those areas presently lacking suitable methodologies are also highlighted. (Author).
Book Synopsis AIAA Aerospace Sciences Meeting and Exhibit, 42nd by :
Download or read book AIAA Aerospace Sciences Meeting and Exhibit, 42nd written by and published by . This book was released on 2004 with total page 618 pages. Available in PDF, EPUB and Kindle. Book excerpt:
