T2-95 Hyperboloid Flare
(Europe)
UPDATED ON 10/15/95
Brief Description
The test is proposed for the validation of Navier-Stokes solvers for
hypersonic viscous flows containing a strong
shock-wave / boundary-layer laminar interaction. The external flow
geometry is axisymmetric.
Focal Point (2.1)
- Numerical
Schwane (fax) +31-1719-85421
- Experimental
Krogmann (fax) +49-551-7092811
Focal Point (2.2)
- Numerical
Schwane (fax) +31-1719-85421
- Experimental
Devezeaux (fax) +33-1-46734149
Full Description
- Preview
full problem description Postscript document.
- Retrieve
compressed Postscript document.
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: Oct. 15, 1995
hsff@math.uh.edu