Longitudinal Aerodynamic Characteristics Of Several High Drag Bodies At Mach Numbers From 150 To 463

Author : James F. Campbell
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.26/5 ( download)

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Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : James F. Campbell
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.83/5 ( download)

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Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : George C. Ashby
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.55/5 ( download)

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Download or read book Longitudinal Aerodynamic Performance of a Series of Power-law and Minimum-wave-drag Bodies at Mach 6 and Several Reynolds Numbers written by George C. Ashby and published by . This book was released on 1974 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Edward J. Ray
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.98/5 ( download)

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Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.14/5 ( download)

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Download or read book STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG written by and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : W. P. Henderson
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.49/5 ( download)

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Download or read book The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93 written by W. P. Henderson and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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ISBN 13 :
Total Pages : 96 pages
Book Rating : 4.57/5 ( download)

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Download or read book Longitudinal Aerodynamic Characteristics of a High-subsonic-speed Transport Airplane Model with a Cambered 40 Deg Sweptback Wing of Aspect Ratio 8 at Mach Numbers to 0.96 written by and published by . This book was released on 1960 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.70/5 ( download)

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Download or read book Longitudinal Aerodynamic Characteristics at a Mach Number of 1.97 of a Series of Related Winged Reentry Configurations for Angles of Attack from 0 Deg to 90 Deg written by and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author :
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.22/5 ( download)

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Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3.00, 3.96, and 4.65 of a Low-fineness-ratio Elliptical Hypersonic Configuration Having Variable-sweep Wing Panels written by and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Edwin E. Davenport
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.76/5 ( download)

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Download or read book Aerodynamic Characteristics of Some Modified Conical Bodies with Low Lift Drag Ratios at Mach Numbers of 2.30 and 4.63 written by Edwin E. Davenport and published by . This book was released on 1972 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: