Design and Evaluation of Active Cooling Systems for Mach 6 Cruise Vehicle Wings PDF Download
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Author: W. A. McConarty
Publisher:
ISBN:
Category : Cooling systems
Languages : en
Pages : 280
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Book 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.
Author: W. A. McConarty
Publisher:
ISBN:
Category : Cooling systems
Languages : en
Pages : 280
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Book 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.
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 978
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340
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Book Description
Author: Richard Hallion
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 698
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Book Description
Author: Richard Hallion
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 696
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Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 276
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340
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Book Description
Author: R. G. Helenbrook
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 140
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Book Description
Results of analytical and design studies are presented for a water-glycol convective cooling system for the airframe structure of a hypersonic transport. System configurations and weights are compared. The influences of system pressure drop and flow control schedules on system weight are defined.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1134
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1386
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Book Description
