Evaluation Of Blended Wing Body Combinations With Curved Plan Forms At Mach Numbers Up To 350

Author : George H. Holdaway
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.20/5 ( download)

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Download or read book Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50 written by George H. Holdaway and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Library of Congress Science and Technology Division
Publisher :
ISBN 13 :
Total Pages : 252 pages
Book Rating : 4.95/5 ( download)

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Download or read book List of Selected References on NASA Programs written by Library of Congress Science and Technology Division and published by . This book was released on 1962 with total page 252 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 : 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 : 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 : Charlie M. Jackson
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.49/5 ( download)

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Download or read book A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow written by Charlie M. Jackson and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of the method, experimental measurements of surface pressures, forces, and moments were made on a series of basic wing-body configurations over a Mach number range from 2.5 to 4.5. Comparison of the theoretical estimates with these experimental data generally indicated good agreement for the entire range of configurations and test conditions.

Author :
Publisher :
ISBN 13 :
Total Pages : 1388 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 1967 with total page 1388 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Harvard Lomax
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.94/5 ( download)

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Download or read book Damping-in-roll Calculations for Slender Swept-back Wings and Slender Wing-body Combinations written by Harvard Lomax and published by . This book was released on 1949 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: The damping-in-roll parameter C(iota)(p) is calculated theoretically for triangular wings on cylindrical bodies and for a class of wings with sweptback plan forms. The analysis is based on the usual assumptions of linearized compressible-flow theory together with the added restrictions that at the free-stream Mach number M(omicron) the product of lM(omicron)(2) and the streamwise velocity gradient is small.

Author : Lowell E. Hasel
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.18/5 ( download)

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Download or read book Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 written by Lowell E. Hasel and published by . This book was released on 1952 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Robert S. Osborne
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.03/5 ( 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 1953 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: