Elevated-temperature Properties of Several Titanium Carbide Base Ceramals PDF Download
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Author: George C. Deutsch
Publisher:
ISBN:
Category : Carbides
Languages : en
Pages : 56
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Book Description
On a strength-to-weight ratio basis, ceramals appeared promising as gas-turbine-blade materials in the temperature range of 1600 to 2400 degrees F.
Author: George C. Deutsch
Publisher:
ISBN:
Category : Carbides
Languages : en
Pages : 56
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Book Description
On a strength-to-weight ratio basis, ceramals appeared promising as gas-turbine-blade materials in the temperature range of 1600 to 2400 degrees F.
Author: Raymond S. Gurnick
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 26
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Book Description
Author: M. J. Whitman
Publisher:
ISBN:
Category : Ceramic materials
Languages : en
Pages : 56
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Book Description
The cobalt ceramals were considered better than the tungsten caramals in over-all oxidation resistance and the molybdenum ceramals were inferior to both the cobalt and tungsten ceramals.
Author: H. J. Hamjian
Publisher:
ISBN:
Category : Boron compounds
Languages : en
Pages : 30
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Book Description
The experiments conducted with boron carbide and each of four metals showed that nickel, cobalt, and iron formed a bonding zone between the metal and the ceramic and that chromium showed satisfactory physical wetting characteristics on the ceramic.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 460
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Book Description
Author:
Publisher:
ISBN:
Category : Energy development
Languages : en
Pages : 64
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 620
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: Frank S. Malvestuto
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 842
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Book Description
Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
