Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722879662
Category :
Languages : en
Pages : 38
Book Description
Some recent developments in the state of the art in missile aerodynamics are reviewed. Among the subjects covered are: (1) tri-service/NASA data base, (2) wing-body interference, (3) nonlinear controls, (4) hypersonic transition, (5) vortex interference, (6) airbreathers, supersonic inlets, (7) store separation problems, (8) correlation of missile data, (9) CFD codes for complete configurations, (10) engineering prediction methods, and (11) future configurations. Suggestions are made for future research and development to advance the state of the art of missile aerodynamics. Nielsen, Jack N. Ames Research Center ...
The Present Status and the Future of Missile Aerodynamics
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722879662
Category :
Languages : en
Pages : 38
Book Description
Some recent developments in the state of the art in missile aerodynamics are reviewed. Among the subjects covered are: (1) tri-service/NASA data base, (2) wing-body interference, (3) nonlinear controls, (4) hypersonic transition, (5) vortex interference, (6) airbreathers, supersonic inlets, (7) store separation problems, (8) correlation of missile data, (9) CFD codes for complete configurations, (10) engineering prediction methods, and (11) future configurations. Suggestions are made for future research and development to advance the state of the art of missile aerodynamics. Nielsen, Jack N. Ames Research Center ...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722879662
Category :
Languages : en
Pages : 38
Book Description
Some recent developments in the state of the art in missile aerodynamics are reviewed. Among the subjects covered are: (1) tri-service/NASA data base, (2) wing-body interference, (3) nonlinear controls, (4) hypersonic transition, (5) vortex interference, (6) airbreathers, supersonic inlets, (7) store separation problems, (8) correlation of missile data, (9) CFD codes for complete configurations, (10) engineering prediction methods, and (11) future configurations. Suggestions are made for future research and development to advance the state of the art of missile aerodynamics. Nielsen, Jack N. Ames Research Center ...
The Present Status and the Future of Missile Aerodynamics
Scientific and Technical Aerospace Reports
Proceedings of the Special Course on Missile Aerodynamics, Held in Rhode-Saint-Genese, Belgium on 30 March-3 April 1987, Held in Athens, Greece on 18-19 May 1987 Held in Ankara, Turkey on 21-22 May 1987
Author: ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRAN CE)
Publisher:
ISBN:
Category :
Languages : en
Pages : 475
Book Description
This course of 12 lectures presents the current state of the art in fundamental knowledge and in practical predictive methods in tactical missile aerodynamics. The first lecture surveys aerodynamic problems encountered on existing and future missiles and the most important predictive methods. A lecture follows on the criteria that define the required prediction accuracy in terms of allowable errors in missile performance and design parameters. The 3rd lecture covers nonlinear aerodynamic effects including formation of flow separation vortices, vortex wakes and vortical interference, and nonlinear compressibility due to presence of shocks. Several lectures present engineering computation methods used for calculating stability and control for conventional and unconventional missiles, illustrated by numerous practical examples. They fall into two categories: semi-empirical methods based on the equivalent angle-of-attack concept and numerical methods, much more recent, based on the resolution of the steady and the unsteady Euler equations with flow separation vortices. Prediction of dynamic derivatives is also presented with a description of the experimental methods. An extensive lecture describes the role of the intake in the propulsion system of turbojet and ramjet powered missiles and addresses both the internal and external aerodynamic aspects of the induction system. A computer aided design procedure for use in conceptual design for sizing and shaping supersonic airbreathing missiles is presented. The prediction of aerodynamic heating and base flows with and without propulsion, and the design of the next generation supersonic and hypersonic missiles are discussed. (edc).
Publisher:
ISBN:
Category :
Languages : en
Pages : 475
Book Description
This course of 12 lectures presents the current state of the art in fundamental knowledge and in practical predictive methods in tactical missile aerodynamics. The first lecture surveys aerodynamic problems encountered on existing and future missiles and the most important predictive methods. A lecture follows on the criteria that define the required prediction accuracy in terms of allowable errors in missile performance and design parameters. The 3rd lecture covers nonlinear aerodynamic effects including formation of flow separation vortices, vortex wakes and vortical interference, and nonlinear compressibility due to presence of shocks. Several lectures present engineering computation methods used for calculating stability and control for conventional and unconventional missiles, illustrated by numerous practical examples. They fall into two categories: semi-empirical methods based on the equivalent angle-of-attack concept and numerical methods, much more recent, based on the resolution of the steady and the unsteady Euler equations with flow separation vortices. Prediction of dynamic derivatives is also presented with a description of the experimental methods. An extensive lecture describes the role of the intake in the propulsion system of turbojet and ramjet powered missiles and addresses both the internal and external aerodynamic aspects of the induction system. A computer aided design procedure for use in conceptual design for sizing and shaping supersonic airbreathing missiles is presented. The prediction of aerodynamic heating and base flows with and without propulsion, and the design of the next generation supersonic and hypersonic missiles are discussed. (edc).
Missile Aerodynamics
Missile Aerodynamics - Dim Past and Indefinite Future
Author: Jack N. Nielsen
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
The present paper covers two distinctly different subjects. The first subject is the efforts of the U.S. Navy and the U.S. Army to develop aerial torpedos during World War I. The Navy team had such prominent engineers as Elmer and Lawrence Sperry and Glenn Curtis. The Army team included Charles F. Kettering and Orville Wright. Despite these eminent personalities, a successful aerial torpedo was not developed for use in World War I. The second subject area covered in the paper is suggestions for future work in missile aerodynamics. High angle of attack aerodynamics, engine-airframe integration and autopilot-airframe integration are covered. In addition, the future of asymmetric vortices, external stores, and computational fluid dynamics are discussed. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 37
Book Description
The present paper covers two distinctly different subjects. The first subject is the efforts of the U.S. Navy and the U.S. Army to develop aerial torpedos during World War I. The Navy team had such prominent engineers as Elmer and Lawrence Sperry and Glenn Curtis. The Army team included Charles F. Kettering and Orville Wright. Despite these eminent personalities, a successful aerial torpedo was not developed for use in World War I. The second subject area covered in the paper is suggestions for future work in missile aerodynamics. High angle of attack aerodynamics, engine-airframe integration and autopilot-airframe integration are covered. In addition, the future of asymmetric vortices, external stores, and computational fluid dynamics are discussed. (Author).
Tactical Missile Aerodynamics
Author: Michael J. Hemsch
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 774
Book Description
This two-volume set includes discussions of the physics of the fluid mechanics phenomena associated with tactical missile flight and the full range of prediction methods required to analyze current and future missiles. It's a valuable resource for missile aerodynamicists, designers, and researchers.
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 774
Book Description
This two-volume set includes discussions of the physics of the fluid mechanics phenomena associated with tactical missile flight and the full range of prediction methods required to analyze current and future missiles. It's a valuable resource for missile aerodynamicists, designers, and researchers.
Air and Missile Defense Systems Engineering
Author: Warren J. Boord
Publisher: CRC Press
ISBN: 1439806713
Category : Technology & Engineering
Languages : en
Pages : 268
Book Description
Air and Missile Defense Systems Engineering fills a need for those seeking insight into the design procedures of the air and missile defense system engineering process. Specifically aimed at policy planners, engineers, researchers, and consultants, it presents a balanced approach to negating a target in both natural and electronic attack environmen
Publisher: CRC Press
ISBN: 1439806713
Category : Technology & Engineering
Languages : en
Pages : 268
Book Description
Air and Missile Defense Systems Engineering fills a need for those seeking insight into the design procedures of the air and missile defense system engineering process. Specifically aimed at policy planners, engineers, researchers, and consultants, it presents a balanced approach to negating a target in both natural and electronic attack environmen
NASA Tech Briefs
Missile Aerodynamics
Author: M. R. Mendenhall
Publisher:
ISBN: 9780962062919
Category : History
Languages : en
Pages :
Book Description
Publisher:
ISBN: 9780962062919
Category : History
Languages : en
Pages :
Book Description