Theory and Analysis of the Dynamic Stability of Missiles PDF Download
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Author: Robert L. Swaim
Publisher:
ISBN: 9781934939437
Category : Science
Languages : en
Pages : 144
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Book Description
Chapter titles are ...(1) Introduction ...(2) Analysis: Thrust Forces and Moments ...(3) Sloshing Propellant Forces and Moments ...(4) Engine Inertia Forces and Moments ...(5) Aerodynamic Forces and Moments ...(6) References ...(7) Appendix A: Structural Dynamics ...(8) Appendix B: Engine Inertia ...(9) Appendix uFuel Sloshing ...(10) Appendix D: Aerodynamic Forces ...(11) Appendix E: Determinant Elements.
Author: Robert L. Swaim
Publisher:
ISBN: 9781934939437
Category : Science
Languages : en
Pages : 144
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Book Description
Chapter titles are ...(1) Introduction ...(2) Analysis: Thrust Forces and Moments ...(3) Sloshing Propellant Forces and Moments ...(4) Engine Inertia Forces and Moments ...(5) Aerodynamic Forces and Moments ...(6) References ...(7) Appendix A: Structural Dynamics ...(8) Appendix B: Engine Inertia ...(9) Appendix uFuel Sloshing ...(10) Appendix D: Aerodynamic Forces ...(11) Appendix E: Determinant Elements.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 980
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Book Description
Author:
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 1118
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Book Description
Author: Robert C. Nelson
Publisher:
ISBN:
Category : History
Languages : en
Pages : 464
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Book Description
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 430
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Book Description
Author: Thomas R. Yechout
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
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Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1196
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Book Description
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1766
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Book Description
Author: Jack Norman Nielsen
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9780962062902
Category : Guided missiles
Languages : en
Pages : 450
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Book Description
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: American Society for Engineering Education
Publisher:
ISBN:
Category : Engineering
Languages : en
Pages : 462
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Book Description
