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

W. A. McConarty
4.9/5 (14242 ratings)
Description: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.We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Design and Evaluation of Active Cooling Systems for Mach 6 Cruise Vehicle Wings. To get started finding Design and Evaluation of Active Cooling Systems for Mach 6 Cruise Vehicle Wings, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
280
Format
PDF, EPUB & Kindle Edition
Publisher
Release
1971
ISBN
h2R_e1FW4XkC

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

W. A. McConarty
4.4/5 (1290744 ratings)
Description: 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.We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with Design and Evaluation of Active Cooling Systems for Mach 6 Cruise Vehicle Wings. To get started finding Design and Evaluation of Active Cooling Systems for Mach 6 Cruise Vehicle Wings, you are right to find our website which has a comprehensive collection of manuals listed.
Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
280
Format
PDF, EPUB & Kindle Edition
Publisher
Release
1971
ISBN
h2R_e1FW4XkC
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