The unsteady flow field about a right circular cone in unsteady flight.

Autoria(s): Brong, E. A.; Air Force Flight Dynamics Laboratory (U.S.) Wright-Patterson Air Force Base, Ohio. Research and Technology Division.; General Electric Company. Reentry Systems Dept.
Data(s)

31/12/1969
Resumo

"These studies were conducted by the General Electric Company, Reentry Systems Department, for the Stability and Control Section of the Flight Dynamics Laboratory of the Air Force Research and Technology Division."

Mode of access: Internet.
Formato

bib
Identificador

http://hdl.handle.net/2027/coo.31924004659540
Idioma(s)

eng
Publicador

[Wright-Patterson Air Force Base, Ohio, Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command,
Direitos

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Palavras-Chave #Boundary value problems #Perturbation (Mathematics) #Aerodynamics
Tipo

text
Acesso ao item digital