Static Aerodynamic Characteristics Of A Single Stage To Orbit Vehicle With Low Planform Loading At Mach Numbers From 03 To 463

Author : Delma C. Freeman
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.10/5 ( download)

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Download or read book Static Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle with Low Planform Loading at Mach Numbers from 0.3 to 4.63 written by Delma C. Freeman and published by . This book was released on 1977 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Delma C. Freeman
Publisher :
ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.83/5 ( download)

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Download or read book Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 written by Delma C. Freeman and published by . This book was released on 1977 with total page 66 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 : Delma C. Freeman
Publisher :
ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.61/5 ( download)

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Download or read book Static Aerodynamic Characeristics of a Winged Single-stage-to-orbit Vehicle at Mach Numbers from 0.3 to 4.63 written by Delma C. Freeman and published by . This book was released on 1978 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Peter T. Bernot
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.19/5 ( download)

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Download or read book Effect of Modifications on Aerodynamic Characteristics of a Single-stage-to-orbit Vehicle at Mach 5.9 written by Peter T. Bernot and published by . This book was released on 1983 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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ISBN 13 :
Total Pages : 514 pages
Book Rating : 4.77/5 ( download)

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Download or read book International Aerospace Abstracts written by and published by . This book was released on 1996 with total page 514 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 : Dennis E. Fuller
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.51/5 ( download)

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Download or read book Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1.57 to 4.65 written by Dennis E. Fuller and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Thomas C. Kelly
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.50/5 ( download)

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Download or read book Aerodynamic Loading Characteristics at Mach Numbers from 0.80 to 1.20 of a 1/10-scale Three-stage Scout Model written by Thomas C. Kelly and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic loads results have been obtained in the Langley 8-foot transonic pressure tunnel at Mach numbers from 0.80 to 1.20 for a 1/10-scale model of the upper three stages of the Scout vehicle. Tests were conducted through an angle-of-attack range from -8° to 8° at an average test Reynolds number per foot of about 4.0 x 106. Results indicated that the peak negative pressures associated with expansion corners at the nose and transition flare exhibit sizeable variations which occur over a relatively small Mach number range. The magnitude of the variations may cause the critical local loading condition for the full-scale vehicle to occur at a Mach number considerably lower than that at which the maximum dynamic pressure occurs in flight. The addition of protuberances simulating antennas and wiring conduits had slight, localized effects. The lift carryover from the nose and transition flare on the cylindrical portions of the model generally increased with an increase in Mach number.

Author :
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ISBN 13 :
Total Pages : 1466 pages
Book Rating : 4.01/5 ( download)

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Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1966 with total page 1466 pages. Available in PDF, EPUB and Kindle. Book excerpt: