Investigation Of Feasibility Of Utilizing Available Heat Resistant Materials For Hypersonic Leading Edge Applications Volume 4 Thermal Properties Of Molybdenum Alloy And Graphite PDF Download

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Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Tests of molybdenum and graphite leading edge components, by Frank M. Anthony and Andrew L. Mistretta

Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Tests of molybdenum and graphite leading edge components, by Frank M. Anthony and Andrew L. Mistretta
Author: Bell Aircraft Corporation
Publisher:
Total Pages: 280
Release: 1961
Genre: Aerodynamics, Hypersonic
ISBN:

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Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Screening test results and selection of materials, by Frank M. Anthony and Harry A. Pearl.v. 6. Determination and design application of mechanical properities of bare and coated graphite, by Alfred Rudnick, Robert L. Carlson, and George K. Manning

Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Screening test results and selection of materials, by Frank M. Anthony and Harry A. Pearl.v. 6. Determination and design application of mechanical properities of bare and coated graphite, by Alfred Rudnick, Robert L. Carlson, and George K. Manning
Author: Bell Aircraft Corporation
Publisher:
Total Pages: 388
Release: 1960
Genre: Aerodynamics, Hypersonic
ISBN:

Download Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Screening test results and selection of materials, by Frank M. Anthony and Harry A. Pearl.v. 6. Determination and design application of mechanical properities of bare and coated graphite, by Alfred Rudnick, Robert L. Carlson, and George K. Manning Book in PDF, ePub and Kindle


Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Analytical methods and design studies, by F. M. Anthony and others

Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Analytical methods and design studies, by F. M. Anthony and others
Author: Bell Aircraft Corporation
Publisher:
Total Pages: 480
Release: 1961
Genre: Aerodynamics, Hypersonic
ISBN:

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Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Oxidation resistance of bare and coated molybdenum alloy and graphite, by Donald J. Powers and others

Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications: Oxidation resistance of bare and coated molybdenum alloy and graphite, by Donald J. Powers and others
Author: Bell Aircraft Corporation
Publisher:
Total Pages: 228
Release: 1960
Genre: Aerodynamics, Hypersonic
ISBN:

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Investigation of Feasibility of Utilizing Available Heat-resistant Materials for Hypersonic Leading-edge Applications. Volume Vi. Determination and Design Application of Mechanical Properties of Bare and Coated Graphite

Investigation of Feasibility of Utilizing Available Heat-resistant Materials for Hypersonic Leading-edge Applications. Volume Vi. Determination and Design Application of Mechanical Properties of Bare and Coated Graphite
Author: ALFRED. RUDNICK
Publisher:
Total Pages: 1
Release: 1960
Genre:
ISBN:

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COATINGS, Stresses, Deformation, Tests, Temperature, Silicon compounds, Carbides, Nitrides, Tensile properties. The results of a study on the mechanical properties of a siliconized Grade ATJ graphite are presented. The mechanical properties were studied as functions of temperature (to 2950 F), strain rate, size, and stress state. Supplementary studies were conducted to determine the room-temperature properties of the uncoated material and the degree of anisotropy of both the coated and uncoated material. Gross variations in the material tended to obscure the effects of the parameters under consideration. With proper selection of material quality, the siliconized Grade ATJ graphite may be used effectively as a structural component at elevated temperature in an oxidizing atmosphere. (Author).


Technical Abstract Bulletin

Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)
Publisher:
Total Pages: 1116
Release: 1961-02
Genre: Technology
ISBN:

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