Aerodynamic Characteristics Of Two Delta Wings And Two Trapezoidal Wings At Mach Number Of 404

Author : Robert W. Dunning
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.99/5 ( download)

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Download or read book Aerodynamic Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number of 4.04 written by Robert W. Dunning and published by . This book was released on 1953 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Emma Jean Landrum
Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.49/5 ( download)

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Download or read book A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes written by Emma Jean Landrum and published by . This book was released on 1962 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Edward F. Ulmann
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.21/5 ( download)

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Download or read book Aerodynamic Characteristics of Two Delta Wings at Mach Number 4.04 and Correlations of Lift and Minimum-drag Data for Delta Wings at Mach Numbers from 1.62 to 6.9 written by Edward F. Ulmann and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Edward F. Ulmann
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.80/5 ( download)

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Download or read book Aerodynamics Characteristics of Two Delta Wings at Mach Number 4.04 and Correlations of Lift and Minimum-drag Data for Delta Wings at Mach Numbers from 1.62 to 6.9 written by Edward F. Ulmann and published by . This book was released on 1952 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Fred M. Smith
Publisher :
ISBN 13 :
Total Pages : 27 pages
Book Rating : 4.37/5 ( download)

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Download or read book Experimental and Theoretical Aerodynamic Characteristics of Two Low-aspect-ratio Delta Wings at Angles of Attack to 50 Degrees at Mach Number of 4.07 written by Fred M. Smith and published by . This book was released on 1957 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Emma Jean Landrum
Publisher :
ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.12/5 ( download)

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Download or read book A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes written by Emma Jean Landrum and published by . This book was released on 1962 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Theodore J. Goldberg
Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.15/5 ( download)

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Download or read book Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations written by Theodore J. Goldberg and published by . This book was released on 1969 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hypersonic aerodynamic characteristics of delta wing x- 15 airplane configurations.

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 : 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 : Mitchel H. Bertram
Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.58/5 ( download)

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Download or read book Investigation of the Aerodynamic Characteristics at High Supersonic Mach Numbers of a Family of Delta Wings Having Double-wedge Sections with the Maximum Thickness at 0.18 Chord written by Mitchel H. Bertram and published by . This book was released on 1954 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: A program to investigate the aerodynamic characteristics of a family of delta wings with a blunt double-wedge section has been conducted at the Langley 11-inch hypersonic tunnel. These wings had a maximum thickness of 8 percent of the chord located at the 18-percent-chord point. For the wings tested at a Mach number of 6.9, the semiapex angle was varied from 5 to 30 degrees and the wings were tested over a range of angle of attack from 0 to 28 degrees and Reynolds numbers in the range of 800,000 to 3,600,000 based on root chord. In addition, pertinent results from tests at Mach number as low as 1.62 have been utilized. The shock-expansion theory and the Newtonian impact theory have been used to analyze the effects of changes made in the various parameters investigated.