Aerodynamic Characteristics of Low Aspect Ratio Fins at Mach Numbers from 0.80 to 1.30 PDF Download
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Author: D.K. Smith
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 166
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Book Description
Author: D.K. Smith
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 166
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Book Description
Author: J. M. Whoric
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 154
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1330
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Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 2106
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Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 446
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Book Description
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).
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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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.
