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Aerodynamic Characteristics Of A Hypersonic Research Airplane Concept Having A 70 Swept Double Delta Wing At Mach Numbers From 150 To 286
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Book Synopsis Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 1.50 to 2.86 by : Jim A. Penland
Download or read book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 1.50 to 2.86 written by Jim A. Penland and published by . This book was released on 1975 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Number 0.2 by : Jim A. Penland
Download or read book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Number 0.2 written by Jim A. Penland and published by . This book was released on 1978 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Delta Wing by :
Download or read book Low-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Delta Wing written by and published by . This book was released on 1974 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70 ̊swept delta wing by : Louis E. Clark
Download or read book Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70 ̊swept delta wing written by Louis E. Clark and published by . This book was released on 1977 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Low-speed and Calculated High-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 65 ̊swept Delta Wing by : Jim A. Penland
Download or read book Experimental Low-speed and Calculated High-speed Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 65 ̊swept Delta Wing written by Jim A. Penland and published by . This book was released on 1974 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow by : Mitchel H. Bertram
Download or read book An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow written by Mitchel H. Bertram and published by . This book was released on 1963 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented for a study of the pressure and heat-transfer distributions and force characteristics of slab delta wings of 70° sweep at Mach numbers of 6.8 and 9.6 in air and 18 in helium. The wings had cylindrical leading edges and were tested with two different noses. One was sharp in plan view and the other was a tangent sphere with the same diameter as the cylindrical leading edge. Simple approaches to predicting the heat transfer are shown to be successful if the flow pattern peculiar to the angle-of-attack range under consideration is taken into account.
Book Synopsis Hypersonic Aerodynamic Characteristics of Two Delta-wing X-15 Airplane Configurations by : Theodore J. Goldberg
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.
Book Synopsis Aerodynamic Characteristics at Mach 6 of a Wing-body Concept for a Hypersonic Research Airplane by : James L. Dillon
Download or read book Aerodynamic Characteristics at Mach 6 of a Wing-body Concept for a Hypersonic Research Airplane written by James L. Dillon and published by . This book was released on 1978 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Configuration at Mach Number 2.20 by : Gerald V. Foster
Download or read book Aerodynamic Characteristics of a Tailless Fixed-wing Supersonic Transport Configuration at Mach Number 2.20 written by Gerald V. Foster and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Number 0.2 of a Wing-body Concept for a Hypersonic Research Airplane by : James L. Dillon
Download or read book Aerodynamic Characteristics at Mach Number 0.2 of a Wing-body Concept for a Hypersonic Research Airplane written by James L. Dillon and published by . This book was released on 1978 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Transonic and Supersonic Speeds of a Rocket-propelled Airplane Configuration Having a Diamond-plan-form Wing Aspect Ration 3.08 and a Low, Swept Horizontal Tail by : Alan B. Kehlet
Download or read book Aerodynamic Characteristics at Transonic and Supersonic Speeds of a Rocket-propelled Airplane Configuration Having a Diamond-plan-form Wing Aspect Ration 3.08 and a Low, Swept Horizontal Tail written by Alan B. Kehlet and published by . This book was released on 1954 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of Wing-body Design Concept for a Hypersonic Research Airplane by : James L. Dillon
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of Wing-body Design Concept for a Hypersonic Research Airplane written by James L. Dillon and published by . This book was released on 1977 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Determination of Damping in Pitch of Swept and Delta Wings at Supersonic Mach Numbers by : John A. Moore
Download or read book Experimental Determination of Damping in Pitch of Swept and Delta Wings at Supersonic Mach Numbers written by John A. Moore and published by . This book was released on 1957 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The damping-in-pitch derivative was determined experimentally at Mach numbers of 2.96 and 3.92 for two delta wings having aspect ratios of 2 and 3 and for one sweptback tapered wing having an aspect ratio of 3 by using a free-oscillation technique. The tests were made at Reynolds numbers based on mean aerodynamic chord from 4,000,000 to 12,000,000 for an angle-of-attack range of zero to 10 degrees. The reduced-frequency parameter ranged from 0.006 to 0.022.
Book Synopsis A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 by : Robert S. Osborne
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:
Book Synopsis The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50° by : John B. McDevitt
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:
Book Synopsis Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 by : William John Small
Download or read book Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 written by William John Small and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
