Static Aerodynamic Characteristics Of Three Rocket Vehicle Configurations At Mach Numbers From 180 To 463 Including Some Effects Of Fin Size Fin Cant And Auxiliary Rocket Motors

Author : Dennis E. Fuller
Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.99/5 ( download)

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Download or read book Static Aerodynamic Characteristics of Three Rocket-vehicle Configurations at Mach Numbers from 1.80 to 4.63 Including Some Effects of Fin Size, Fin Cant, and Auxiliary Rocket Motors written by Dennis E. Fuller and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Clarence A. Brown
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.53/5 ( download)

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Download or read book Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 written by Clarence A. Brown and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Joseph A. Yuska
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.62/5 ( download)

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Download or read book Static Aerodynamic Characteristics of a Rocket Vehicle with Thick Wedge Fins and Sweptback Leading and Trailing Edges written by Joseph A. Yuska and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The longitudinal static stability characteristics of three one-fifth scale models of the second stage of a sounding rocket were calculated and compared with the measured values at Mach numbers of 1.79 to 3.47. All three models had fins of trapezoidal planform with sweptback leading and trailing edges, small aspect ratio, and thick wedge sections, but differed in fin area and overall model length. Calculation of center of pressure and normal-force coefficient slope at zero normal force were in good agreement with experimental data.

Author : Ross B. Robinson
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.24/5 ( download)

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Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : John T. Suttles
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.86/5 ( download)

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Download or read book Aerodynamic Characteristics from Mach 0.22 to 4.65 of a Two-stage Rocket Vehicle Having an Unusual Nose Shape written by John T. Suttles and published by . This book was released on 1964 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : William F. Hinson
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.73/5 ( download)

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Download or read book Aerodynamic Characteristics in Pitch of a 1/7-scale Model of a Two- and Three-stage Rocket Configuration at Mach Numbers of 0.4 to 4.63 written by William F. Hinson and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63.

Author : Thomas C. Kelly
Publisher :
ISBN 13 :
Total Pages : 74 pages
Book Rating : 4.45/5 ( download)

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Download or read book Transonic Wind-tunnel Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Configurations of the Scout Vehicle and of a Number of Related Models written by Thomas C. Kelly and published by . This book was released on 1961 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results have been obtained i n t h e Langley 8-foot transonic pressure tunnel at Mach numbers from 0.40 t o 1.20 for several configurations of the Scout vehicle and f o r a number of related models. Tests extended over an angle-of-attack range from about -10 degrees to 10 degrees at a Reynolds number per foot of about 3.8 x 10 sup 6.

Author : Clyde Hayes
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.11/5 ( download)

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Download or read book Supersonic Aerodynamic Characteristics of a 1/6-scale Model of the Final Two Stages of the Argo D-4 Four-stage Rocket Vehicle written by Clyde Hayes and published by . This book was released on 1965 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Earl D. Knechtel
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.95/5 ( download)

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Download or read book Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.

Author : E. S. Washington
Publisher :
ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.36/5 ( download)

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Download or read book Aerodynamic and Cold Jet Plume Geometry Characteristics of the Army Free Rocket at Transonic Mach Numbers written by E. S. Washington and published by . This book was released on 1975 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt: