Extrait de : AIAA/ASME/SAE 27th Joint propulsion conference and exhibit, Sacramento CA, June 24-27, 1991Available at INIST (FR), Document Supply Service, under shelf-number : 22419, issue : a.1991 v.129 / INIST-CNRS - Institut de l'Information Scientifique et TechniqueSIGLEFRFranc
Communication to : 37th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Salt Lake City (...
The present analytical, numerical, and experimental investigations are performed to study the flow f...
An efficient Navier-Stokes analysis was successfully applied to simulate the complex flow field in t...
Communication to : 2nd spatial solid rocket propulsion symposium, Rome (Italie), November 21-24, 200...
Published in : 40th AIAA aerospace science meeting + exhibit, Reno (USA), January 14-17, 2002SIGLEAv...
La caractérisation et la simulation des écoulements internes au sein des moteurs àpropergol solide, ...
The flowfield inside the second solid stage of the European launch vehicle VEGA is simulated with a ...
Communication to : 6th International congress on sound and vibration, Lyngby (Denmark), July 05-08, ...
A mathematical analysis and a computer program based upon that analysis are presented for calculatin...
Communication to : 2nd spatial solid rocket propulsion symposium, Roma (Italy), November 21-24, 2000...
We explore the potential of the immersed boundary (IB) method to predict pressure oscillations in so...
The ability to accurately model the operation of a solid rocket motor before undergoing multiple fir...
A time-resolved numerical analysis of combustion dynamics of double-base homogenous solid propellant...
High frequency combustion instabilities imply a major risk for the solid rocket motor's stable opera...
Traditionally, Solid Rocket Motor (SRM) internal ballistic performance has been analyzed and predict...
Communication to : 37th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Salt Lake City (...
The present analytical, numerical, and experimental investigations are performed to study the flow f...
An efficient Navier-Stokes analysis was successfully applied to simulate the complex flow field in t...
Communication to : 2nd spatial solid rocket propulsion symposium, Rome (Italie), November 21-24, 200...
Published in : 40th AIAA aerospace science meeting + exhibit, Reno (USA), January 14-17, 2002SIGLEAv...
La caractérisation et la simulation des écoulements internes au sein des moteurs àpropergol solide, ...
The flowfield inside the second solid stage of the European launch vehicle VEGA is simulated with a ...
Communication to : 6th International congress on sound and vibration, Lyngby (Denmark), July 05-08, ...
A mathematical analysis and a computer program based upon that analysis are presented for calculatin...
Communication to : 2nd spatial solid rocket propulsion symposium, Roma (Italy), November 21-24, 2000...
We explore the potential of the immersed boundary (IB) method to predict pressure oscillations in so...
The ability to accurately model the operation of a solid rocket motor before undergoing multiple fir...
A time-resolved numerical analysis of combustion dynamics of double-base homogenous solid propellant...
High frequency combustion instabilities imply a major risk for the solid rocket motor's stable opera...
Traditionally, Solid Rocket Motor (SRM) internal ballistic performance has been analyzed and predict...
Communication to : 37th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, Salt Lake City (...
The present analytical, numerical, and experimental investigations are performed to study the flow f...
An efficient Navier-Stokes analysis was successfully applied to simulate the complex flow field in t...
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