The Present Status and the Future of Missile Aerodynamics
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Total Pages | : 42 |
Release | : 1988 |
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Total Pages | : 42 |
Release | : 1988 |
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Author | : Jack N. Nielsen |
Publisher | : |
Total Pages | : 37 |
Release | : 1981 |
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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).
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Total Pages | : 356 |
Release | : 1974 |
Genre | : Aerodynamics |
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Author | : National Aeronautics and Space Adm Nasa |
Publisher | : Independently Published |
Total Pages | : 38 |
Release | : 2018-10-15 |
Genre | : Science |
ISBN | : 9781728741178 |
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
Author | : Mark Pinney |
Publisher | : McGraw-Hill Professional |
Total Pages | : 0 |
Release | : 2013-12-29 |
Genre | : Technology & Engineering |
ISBN | : 9780071831321 |
Proven techniques for deriving the basic aerodynamic properties of axisymmetric-shaped bodies with the minimum amount of time and effort Aerodynamics of Missiles and Rockets describes the basic aerodynamics model used in the widespread Analytical Initial Missile Synthesis (AIMS) computer code for symmetric missile and rocket sizing and design. It is a collection of empirical, semi-empirical and theoretical aerodynamics engineering methods for a component build-up approach to aerodynamics prediction. This book serves as an on-the-job application manual and desk reference for the prediction of basic aerodynamics. It can also be used for courses in applied aerodynamics in Mechanical and Aerospace Engineering programs and for short courses in industry and government. This practical guide provides an alternative approach to utilizing numerous, complex, stand-alone computer codes, but is also a good complement to these codes. The book offers insight into the methods and techniques used to derive answers and correct magnitudes generated by code, giving confidence in final results. Features a Microsoft Excel file that automates calculations and provides complete tabulated output for missile and rocket geometry and design, and design and for rapid assessments of aerodynamic properties based on changes in geometry or flight conditions On-the-job application manual and desk reference for the prediction of basic aerodynamics Combination of long-standing, empirical and semi-empirical techniques with classical aerodynamic theory A component build-up approach utilized, with body and wing/tail surface aerodynamics determined separately and then combined for total configuration zero-lift drag, lift, center of pressure location, and pitching moment
Author | : M. R. Mendenhall |
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Total Pages | : |
Release | : 1989-01-01 |
Genre | : History |
ISBN | : 9780962062919 |
Author | : Jack Norman Nielsen |
Publisher | : AIAA (American Institute of Aeronautics & Astronautics) |
Total Pages | : 450 |
Release | : 1988-01-01 |
Genre | : Guided missiles |
ISBN | : 9780962062902 |
The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. " Missile Aerodynamics," a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.
Author | : J. N. Nielsen |
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Total Pages | : |
Release | : 1960 |
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Author | : Michael R. Mendenhall |
Publisher | : |
Total Pages | : 623 |
Release | : 1989 |
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Contents: A Survey of Missile Aerodynamics; Missile Dynamics: A Critical Assessment of Prediction Capabilities; Appropriate Aeroprediction Accuracy in Defining Missile Systems for Aerodynamic Flight; Application of Experimental Techniques to Store Release Problems; Use of Semiempirical Aerodynamic Methods for Preliminary Design; The Role of Computational Fluid Dynamics in Missile Aerodynamics; A Review of High-Speed, Convective, Heat-Transfer Computation Methods; Prediction Methods For Store Separation; High Performance Missiles of the Future; The Use of Lateral Jet Control at Aerospatiale; The Integration of Stores on Modern Tactical Aircraft. Where We Have Been, and What We Should Do For the Future; VLA Missile Development and High Angle of Attack Behavior; and Dynamic Derivations of Missiles and Fighter-Type Configurations at High Angles of Attack. (JHD).