Name: Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins from Mach 0.60 to 4.63
Price: 31.19 EUR
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Author: Allen, Jerry M. ; Nasa Technical Reports Server (Ntrs)
ISBN: 9781287257585

portada Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins from Mach 0.60 to 4.63

Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins from Mach 0.60 to 4.63

Type

Physical Book

Author

Nasa Technical Reports Server (Ntrs)

Jerry M. Allen

Publisher

Bibliogov

Language

English

Pages

118

Format

Paperback

Dimensions

24.6 x 18.9 x 0.6 cm

Weight

0.23 kg.

ISBN13

9781287257585

Synopsis "Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins from Mach 0.60 to 4.63"

An experimental study has been performed to develop a large force and moment aerodynamic data set on a slender axisymmetric missile configuration having cruciform strakes and in-line control tail fins. The data include six-component balance measurements of the configuration aerodynamics and three-component measurements on all four tail fins. The test variables include angle of attack, roll angle, Mach number, model buildup, strake length, nose size, and tail fin deflection angles to provide pitch, yaw, and roll control. Test Mach numbers ranged from 0.60 to 4.63. The entire data set is presented on a CD-ROM that is attached to this paper. The CD-ROM also includes extensive plots of both the six-component configuration data and the three-component tail fin data. Selected samples of these plots are presented in this paper to illustrate the features of the data and to investigate the effects of the test variables.

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Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins from Mach 0.60 to 4.63 - Allen, Jerry M. ; Nasa Technical Reports Server (Ntrs)

Synopsis "Aerodynamics of an Axisymmetric Missile Concept Having Cruciform Strakes and In-Line Tail Fins from Mach 0.60 to 4.63"

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