Aerodynamic Characteristics Of Several Cranked Leading Edge Wing Body Combinations At Mach Numbers From 04 To 294

Author : Edward J. Hopkins
Publisher :
ISBN 13 :
Total Pages : 98 pages
Book Rating : 4.98/5 ( download)

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Download or read book Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94 written by Edward J. Hopkins and published by . This book was released on 1967 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Odell A. Morris
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.59/5 ( download)

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Download or read book Aerodynamic Characteristics in Pitch of Several Ring-wing-body Configurations at a Mach Number of 2.2 written by Odell A. Morris and published by . This book was released on 1962 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Odell A. Morris
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.44/5 ( download)

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Download or read book Aerodynamic Characteristics in Pitch of Several M-wing-body Combinations at Mach Numbers of 2.40, 2.60, and 2.86 written by Odell A. Morris and published by . This book was released on 1965 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : John E. Lamar
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.78/5 ( download)

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Download or read book Aerodynamic-center Considerations of Wings and Wing-body Combinations written by John E. Lamar and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Robert S. Osborne
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.25/5 ( download)

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Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Robert G. Kyle
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.13/5 ( download)

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Download or read book Effect of Wing Leading-edge Shape on Aerodynamic Characteristics of a 67 ̊swept Wing-body Model at Mach 1.50 to 4.63 written by Robert G. Kyle and published by . This book was released on 1966 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : John B. McDevitt
Publisher :
ISBN 13 :
Total Pages : 114 pages
Book Rating : 4.58/5 ( download)

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Download or read book The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50° written by John B. McDevitt and published by . This book was released on 1960 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Kenneth P. Spreemann
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.82/5 ( download)

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Download or read book Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers of 0.40 to 0.93 of a 45© Sweptback Wing of Aspect Ratio 4 written by Kenneth P. Spreemann and published by . This book was released on 1957 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : William C. Sleeman
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.03/5 ( download)

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Download or read book Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section written by William C. Sleeman and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.

Author :
Publisher :
ISBN 13 :
Total Pages : 540 pages
Book Rating : 4.36/5 ( download)

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Download or read book International Aerospace Abstracts written by and published by . This book was released on 1962 with total page 540 pages. Available in PDF, EPUB and Kindle. Book excerpt: