Investigation of feasibility of utilizing available heat resistant materials for hypersonic leading edge applications.


Autoria(s): Bell Aircraft Corporation.
Data(s)

31/12/1969

Resumo

"Volumes I through VIII are unclassified while volume IX is classified secret."

"USAF Contract AF33(616)-6034."

v. 2. Analytical methods and design studies, by F. M. Anthony and others.--v. 3. 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.--v.7. Oxidation resistance of bare and coated molybdenum alloy and graphite, by Donald J. Powers and others.--v. 8. Tests of molybdenum and graphite leading edge components, by Frank M. Anthony and Andrew L. Mistretta.

Mode of access: Internet.

Formato

bib

bib

bib

bib

bib

Identificador

http://hdl.handle.net/2027/coo.31924004655423

http://hdl.handle.net/2027/coo.31924004655431

http://hdl.handle.net/2027/coo.31924004655449

http://hdl.handle.net/2027/coo.31924004655456

http://hdl.handle.net/2027/coo.31924004655464

Idioma(s)

eng

Publicador

Wright-Patterson Air Force Base, Ohio, Wright Air Development Center, Air Research and Development Command, U. S. Air Force,

Direitos

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Palavras-Chave #Materials at high temperatures #Aerodynamics, Hypersonic #Aerofoils
Tipo

text