Onera - return on innovation
Ligne orange

FRANÇAIS


Search Results

 
Afterbody

Our main pages on this subject:

1.Aerodynamics - Special prize from the ESA for Sébastien Deck
 A special prize from the European Space Agency (ESA) was given to Sébastien Deck, a CFD specialist at Onera, for his contribution to the understanding of flows around launcher afterbodies.... ZDES calculation of the launcher afterbody where we can appreciate the complexity of the flow.... The simulations of Sébastien Deck around the Ariane 5 base has helped to improve understanding of the flows around the launcher afterbody, which has made it possible for the agencies (Esa, Cnes) to better adapt certain instabilities of the launcher (this is why he received the prize)....
 
2.ONERA - Fundamental and Experimental Aerodynamics (DAFE) - References
 Aerodynamics of afterbodies and propulsive nozzles...
 
3.ONERA - Fundamental and Experimental Aerodynamics (DAFE) - Publications
 Analysis of unsteadiness in afterbody transonic flows....
 
4.Base and Afterbody Flow Modelling - ONERA / DAFE-EN
 Base and Afterbody Flow Modelling - ONERA / DAFE-ENWho are we ?Fundamental and Experimental Aerodynamics... Base and Afterbody Flow Modelling. Calculation by Solving of the Navier-Stokes Equations for the Flow Downstream of an Afterbody with Thermal Effects. Isothermal Contours.. Research is actively conducted on base flows, which have practical importance for aircraft, missiles, launchers and projectiles..
 
5.DAFE Computation Codes - ONERA / DAFE-EN
 Low-cost prediction of general aerothermal quantities on projectile or propelled missile afterbodies.... Modelling of turbulent separated flows : afterbody flows and internal flows and jets...
 
6.Fundamental and Experimental Aerodynamics - ONERA / DAFE
 Aerodynamics of Aircraft, Missile and Launcher Afterbodies...
 
7.Microsoft PowerPoint - Onera - 3D separation - 2011 - Part 3
 Afterbody flows... Afterbody flows... 1. Non-propelled afterbody 2. Propelled afterbody without base 3. Propelled afterbody with base 4. Rectangular section afterbody 5. Two-nozzle afterbody 6. Flow past an automobile... Non-propelled axisymmetric afterbody at incidence Skin friction line pattern...
 
8.Microsoft PowerPoint - Onera - 3D separation - 2011 - Part 4
 Propelled afterbody in the Onera-Meudon wind tunnel R1Ch... Axisymmetric afterbody at zero incidence... Non-propelled axisymmetric afterbody at zero incidence... Non-propelled axisymmetric afterbody at zero incidence... Non-propelled axisymmetric afterbody at zero incidence... Non-propelled axisymmetric afterbody at zero incidence...
 
9.S3 Transonic Wind-Tunnel - ATAC Launch Vehicle Afterbody - ONERA / DAFE-EN
 S3 Transonic Wind-Tunnel - ATAC Launch Vehicle Afterbody - ONERA / DAFE-EN... Study of ATAC Launch Vehicle Afterbody...
 
10.Transatmospheric Aircraft (AHYP2)
 An afterbody must be well-designed... The propulsion system and afterbody... These nozzles use the rear part of the spacecraft fuselage, also called afterbody, as an expansion ramp....
 


© ONERA 2007 - Terms of use