T6-95 Propulsion Nozzle Flow
(Europe)
UPDATED ON 09/20/95
UPDATED ON 07/24/95
Brief Description
The test is proposed for code assessment simulating internal
supersonic flow in an axisymmetric propulsion nozzle.
Focal Point
- Numerical
Joubert (fax) +33-60598725
- Experimental
Delery (fax) +33-1-46235151
Full Description
- Preview
full problem description Postscript document.
- Retrieve
compressed Postscript document.
- Preview
geometric description Postscript document.
- Retrieve geometric ascii file "T6_propulsion_nozzle_file_geom_bot".
- Retrieve geometric ascii file "T6_propulsion_nozzle_file_geom_ext".
- Retrieve geometric ascii file "T6_propulsion_nozzle_file_geom_exti".
- Retrieve geometric ascii file "T6_propulsion_nozzle_file_geom_exto".
- Retrieve geometric ascii file "T6_propulsion_nozzle_file_geom_top".
- Retrieve boundary condition ascii file "T6_propulsion_nozzle_bc".
Working Group Chairman
Francesco Grasso
Universita di Roma 'la Sapienza'
Dipartimento di Meccanica e Aeronautica
Via Eudossiana 18, Roma, Italia, 00184
(tel) +39-6-44585202 (fax) +39-6-4881759
e-mail: grasso@grasso.ing.uniroma1.it
Date of last change: July 24, 1995
hsff@math.uh.edu