Author: Bell Aircraft CorpPublisher:
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 CorpPublisher:
ISBN:
Category : Ceramic metals
Languages : en
Pages : 296
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 CorporationPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 480
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 CorporationPublisher:
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 CorporationPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 164
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 CorporationPublisher:
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 CorporationPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 388
Book Description
Technical Abstract Bulletin
Author: A Review of the Air Force Materials Research and Development Program
Author: United States. Wright Air Development DivisionPublisher:
ISBN:
Category : Materials
Languages : en
Pages : 276
Book Description
A review of the research and development work sponsored in the field of materials and processes over the past decade is presented. Abstracts of WADC Technical Reports for the period 1 July 1951 to 30 June 1953 are included. A summary of Technical Reports published in the areas of metallurgy, textiles, petroleum products, structural materials, rubbers, plastics, packaging, protective treatments, analysis and measurements are included also.
A Review of the Air Force Materials Research and Development Program
Author: Donna J. TatePublisher:
ISBN:
Category : Materials
Languages : en
Pages : 262
Book Description
These reports cover basic and applied research in the materials area being conducted by the Metals and Ceramics, Non-metallic Materials, Physics, Manufacturing Technology and Applications Laboratories of the Directorate of Materials and Processes.
Experimental Investigation of Thermal-buckling Characteristics of Flanged, Thin-shell Leading Edges
Author: Jerald M. JenkinsPublisher:
ISBN:
Category : Investigations
Languages : en
Pages : 36
Book Description
The leading edges of winged hypersonic aircraft are known to be subjected to intense aerodynamic heating (ref. 1) in flight. Detailed research investigations into specific types of leading edges suitable for hypersonic use have been limited. The heat-sink concept, although excessive in weight and limited to short durations of heating (ref. 2), has been the most widely used type of leading edge for hypersonic application. Limited experimental and analytical work on shell types of leading edges (refs. 3 and 4) has been conducted; however, the thermal-buckling behavior of leading edges has been defined only in analytical studies, such as references 5 and 6. These theories include simplifying assumptions, which impose limitations on their applicability to design problems. A series of experimental investigations into the thermal-buckling behavior of flanged, thin-shell leading edges has been conducted at the NASA Flight Research Center, Edwards, Calif.