Author: Bell Aircraft Corp
Publisher:
ISBN:
Category : Ceramic metals
Languages : en
Pages : 296
Book Description
Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications
Author: Bell Aircraft Corp
Publisher:
ISBN:
Category : Ceramic metals
Languages : en
Pages : 296
Book Description
Publisher:
ISBN:
Category : Ceramic metals
Languages : en
Pages : 296
Book Description
Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications
Author: Bell Aircraft Corporation
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 164
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 164
Book Description
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:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 480
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 480
Book Description
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:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 280
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 280
Book Description
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:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 388
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 388
Book Description
Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications
Author: Bell Aircraft Corp
Publisher:
ISBN:
Category : Ceramic metals
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Ceramic metals
Languages : en
Pages :
Book Description
Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications. Volume 4. Thermal Properties of Molybdenum Alloy and Graphite
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
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:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 228
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 228
Book Description
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:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 212
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 212
Book Description
Investigation of Feasibility of Utilizing Available Heat Resistant Materials for Hypersonic Leading Edge Applications
Author: Bell Aircraft Corporation
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 252
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 252
Book Description