Hypersonic Cruise Vehicle Wing Structure Evaluation

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Publisher :
ISBN 13 :
Total Pages : 180 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Hypersonic Cruise Vehicle Wing Structure Evaluation by :

Download or read book Hypersonic Cruise Vehicle Wing Structure Evaluation written by and published by . This book was released on 1970 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Substantiation Data for Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 1, Sections 1-10

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Publisher :
ISBN 13 :
Total Pages : 498 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Substantiation Data for Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 1, Sections 1-10 by :

Download or read book Substantiation Data for Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 1, Sections 1-10 written by and published by . This book was released on 1970 with total page 498 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 3, Sections 23-27

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Publisher :
ISBN 13 :
Total Pages : 496 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 3, Sections 23-27 by :

Download or read book Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 3, Sections 23-27 written by and published by . This book was released on 1970 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 2, Sections 11-22

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Publisher :
ISBN 13 :
Total Pages : 584 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 2, Sections 11-22 by :

Download or read book Hypersonic Cruise Vehicle Wing Structure Evaluation - Volume 2, Sections 11-22 written by and published by . This book was released on 1970 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Cruise Vehicle Wing Structure Evaluation

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Publisher :
ISBN 13 :
Total Pages : 180 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Hypersonic Cruise Vehicle Wing Structure Evaluation by :

Download or read book Hypersonic Cruise Vehicle Wing Structure Evaluation written by and published by . This book was released on 1970 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Review of Hypersonic Cruise Vehicles

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Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis A Review of Hypersonic Cruise Vehicles by :

Download or read book A Review of Hypersonic Cruise Vehicles written by and published by . This book was released on 1966 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Evaluation of Structural Design Concepts for an Arrow-wing Supersonic Cruise Aircraft

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Publisher :
ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Evaluation of Structural Design Concepts for an Arrow-wing Supersonic Cruise Aircraft by : I. F. Sakata

Download or read book Evaluation of Structural Design Concepts for an Arrow-wing Supersonic Cruise Aircraft written by I. F. Sakata and published by . This book was released on 1977 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Paper

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Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Technical Paper by :

Download or read book NASA Technical Paper written by and published by . This book was released on 1980 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Structural Weight Analysis of Hypersonic Aircraft

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Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Structural Weight Analysis of Hypersonic Aircraft by : Mark D. Ardema

Download or read book Structural Weight Analysis of Hypersonic Aircraft written by Mark D. Ardema and published by . This book was released on 1972 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Wing Test Structure Design, Analysis, and Fabrication

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Publisher :
ISBN 13 :
Total Pages : 158 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Hypersonic Wing Test Structure Design, Analysis, and Fabrication by :

Download or read book Hypersonic Wing Test Structure Design, Analysis, and Fabrication written by and published by . This book was released on 1973 with total page 158 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Arrow-wing Supersonic Cruise Aircraft Structural Design Concepts Evaluation. Volume 1: Sections 1 Through 6

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Publisher :
ISBN 13 :
Total Pages : 452 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Arrow-wing Supersonic Cruise Aircraft Structural Design Concepts Evaluation. Volume 1: Sections 1 Through 6 by :

Download or read book Arrow-wing Supersonic Cruise Aircraft Structural Design Concepts Evaluation. Volume 1: Sections 1 Through 6 written by and published by . This book was released on 1975 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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Publisher :
ISBN 13 :
Total Pages : 1134 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1989 with total page 1134 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Fuselage/tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles: Structural Analysis

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Publisher :
ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis A Fuselage/tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles: Structural Analysis by :

Download or read book A Fuselage/tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles: Structural Analysis written by and published by . This book was released on 1975 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 910 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1975 with total page 910 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fatigue at Elevated Temperatures

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Publisher : ASTM International
ISBN 13 :
Total Pages : 804 pages
Book Rating : 4./5 ( download)

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Book Synopsis Fatigue at Elevated Temperatures by :

Download or read book Fatigue at Elevated Temperatures written by and published by ASTM International. This book was released on 1973 with total page 804 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Fuselage/tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles--summary

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Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Fuselage/tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles--summary by : C. J. Pirrello

Download or read book A Fuselage/tank Structure Study for Actively Cooled Hypersonic Cruise Vehicles--summary written by C. J. Pirrello and published by . This book was released on 1976 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design and Evaluation of Active Cooling Systems for Mach 6 Cruise Vehicle Wings

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Publisher :
ISBN 13 :
Total Pages : 280 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Design and Evaluation of Active Cooling Systems for Mach 6 Cruise Vehicle Wings by : W. A. McConarty

Download or read book Design and Evaluation of Active Cooling Systems for Mach 6 Cruise Vehicle Wings written by W. A. McConarty and published by . This book was released on 1971 with total page 280 pages. Available in PDF, EPUB and Kindle. Book excerpt: Active cooling systems, which included transpiration, film, and convective cooling concepts, are examined. Coolants included hydrogen, helium, air, and water. Heat shields, radiation barriers, and thermal insulation are considered to reduce heat flow to the cooling systems. Wing sweep angles are varied from 0 deg to 75 deg and wing leading edge radii of 0.05 inch and 2.0 inches are examined. Structural temperatures are varied to allow comparison of aluminum alloy, titanium alloy, and superalloy structural materials. Cooled wing concepts are compared among themselves, and with the uncooled concept on the basis of structural weight, cooling system weight, and coolant weight.