Add to ORKGCommunication to : 12th AIAA International space planes and hypersonic systems and technologies, Norfolk (USA), 15-19 decembre 2003SIGLEAvailable from INIST (FR), Document Supply Service, under shelf-number : 22419, issue : a.2004 n.11 / INIST-CNRS - Institut de l'Information Scientifique et TechniqueFRFranc
"Final report: 15 March 1972 -- 15 May 1974.""June 1975."Includes bibliographical references (pages ...
Communication to : AIAA fluids 2000 conference, Denver (USA), June 19-22, 2000SIGLEAvailable from IN...
Tire de : Symposium UITAM on Aerothermochemistry of Spacecraft and Associated Hypersonic Flow, Marse...
Communication to : 3rd international symposium on atmospheric reentry vehicles and systems, Arcachon...
Communication to : 1st Europe - US high speed flow field - Database workshop CIRA, Naples (Italy), N...
Hypersonics is of current national interest, but improved understanding of fundamental flow physics ...
© 2014 Cambridge University Press. Strong interactions of shock waves with boundary layers lead to f...
An experimental campaign was carried out to investigate transitional shock wave - boundary layer int...
"February 1990."--Cover.Prepared at the Joint Institute for Advancement of Flight Sciences for Langl...
The control surfaces of hypersonic lifting vehicles are some of the hardest parts to design. The rea...
We perform direct numerical simulations of shock-wave/boundary-layer interactions at Mach number M =...
An experimental campaign was carried out to investigate transitional shock wave--boundary layer inte...
textThe mean flowfield and time-dependent characteristics of a Mach 5 cylinder-induced transitional ...
"Prepared for the 29th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics...
Communication to : 21th rarefied gas dynamics symposium, Marseille (France), July 26-31, 1998Availab...
"Final report: 15 March 1972 -- 15 May 1974.""June 1975."Includes bibliographical references (pages ...
Communication to : AIAA fluids 2000 conference, Denver (USA), June 19-22, 2000SIGLEAvailable from IN...
Tire de : Symposium UITAM on Aerothermochemistry of Spacecraft and Associated Hypersonic Flow, Marse...
Communication to : 3rd international symposium on atmospheric reentry vehicles and systems, Arcachon...
Communication to : 1st Europe - US high speed flow field - Database workshop CIRA, Naples (Italy), N...
Hypersonics is of current national interest, but improved understanding of fundamental flow physics ...
© 2014 Cambridge University Press. Strong interactions of shock waves with boundary layers lead to f...
An experimental campaign was carried out to investigate transitional shock wave - boundary layer int...
"February 1990."--Cover.Prepared at the Joint Institute for Advancement of Flight Sciences for Langl...
The control surfaces of hypersonic lifting vehicles are some of the hardest parts to design. The rea...
We perform direct numerical simulations of shock-wave/boundary-layer interactions at Mach number M =...
An experimental campaign was carried out to investigate transitional shock wave--boundary layer inte...
textThe mean flowfield and time-dependent characteristics of a Mach 5 cylinder-induced transitional ...
"Prepared for the 29th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics...
Communication to : 21th rarefied gas dynamics symposium, Marseille (France), July 26-31, 1998Availab...
"Final report: 15 March 1972 -- 15 May 1974.""June 1975."Includes bibliographical references (pages ...
Communication to : AIAA fluids 2000 conference, Denver (USA), June 19-22, 2000SIGLEAvailable from IN...
Tire de : Symposium UITAM on Aerothermochemistry of Spacecraft and Associated Hypersonic Flow, Marse...