Aerodynamic Characteristics From Mach 022 To 465 Of A Two Stage Rocket Vehicle Having An Unusual Nose Shape

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 : 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 : 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 : 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 : William A. Corlett
Publisher :
ISBN 13 :
Total Pages : 106 pages
Book Rating : 4.75/5 ( download)

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Download or read book Effect of First-stage Geometry on Aerodynamic Characteristics in Pitch of Two-stage Rocket Vehicles from Mach 1.57 to 2.86 written by William A. Corlett and published by . This book was released on 1965 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Byron M. Jaquet
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.65/5 ( download)

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Download or read book Aerodynamic Characteristics at a Mach Number of 3.10 of Several Fourth-stage Shapes of the Scout Research Vehicle written by Byron M. Jaquet and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Robert J. Keynton
Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.16/5 ( download)

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Download or read book Investigation of the Aerodynamic Characteristics of Two Preliminary Designs of Scout Research Vehicle at Mach Numbers from 1.77 to 4.65 written by Robert J. Keynton and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Clarence A. Brown
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.45/5 ( download)

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Download or read book Static Aerodynamic Characteristics of a Three-stage Rocket Vehicle Having Various Fin Configurations at Low Subsonic Mach Numbers and Angles of Attack Up to 28 ̊ written by Clarence A. Brown and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : William J. Monta
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.91/5 ( download)

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Download or read book Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins written by William J. Monta and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : CLARENCE A. JR. BROWN
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.67/5 ( 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. JR. BROWN and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted in the Langley Unitary Plan wind tunnel to determine the effects of fin cant and size on the static aerodynamic characteristics of a 0.081-scale model of a three-stage and a two-stage Trailblazer II configuration. Tests were performed at Mach numbers from 1.47 to 4.63 and at a Reynolds number per foot of 3.0 x 10 to the 6th power. he angleof-attack range varied from approximately -5 to 5 degrees and angle of sideslip varied from approximately -4 to 4 degrees. All first-stage fins tested gave adequate static stability when the center-of-gravity travel of the flight model was taken into account. The presence of the auxiliary rocket motors in the lateral plane decreased the effectiveness of the fins in the pitch plane at the lower Mach number and increased the fin effectiveness at the higher Mach numbers. Removal of the auxiliary rocket motors from the first stage of the two-stage configuration reduced the axial force about 25% at the low Mach numbers and about 15% at the high Mach numbers. (Author).