Flow calculation in the high power laser wind tunnel: case of a discharge in a pure supersonic flow
Technical Report
·
OSTI ID:5706845
The flow in the ISL high power CO/sub 2/ laser wind tunnel was investigated taking into consideration phenomena related to the excitation and vibration relaxation of the gas. The calculation was based on a theoretical model leading to a first order differential equation system of classical form which is solved by using the Runge-Kutta method. A detailed description is presented of the FORTRAN 4 computer program written for an IBM 370/135.
- Research Organization:
- Institut Franco-Allemand de Recherches de Saint-Louis, 68 (France)
- DOE Contract Number:
- DRME-74/397
- OSTI ID:
- 5706845
- Report Number(s):
- N-78-22341; ISL-R-101/77
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
42 ENGINEERING
ELECTRIC DISCHARGES
SUPERSONIC FLOW
RUNGE-KUTTA METHOD
CARBON DIOXIDE LASERS
DIFFERENTIAL EQUATIONS
FORTRAN
WIND TUNNELS
EQUATIONS
FLUID FLOW
GAS LASERS
ITERATIVE METHODS
LASERS
NUMERICAL SOLUTION
PROGRAMMING LANGUAGES
TUNNELS
420400* - Engineering- Heat Transfer & Fluid Flow
420300 - Engineering- Lasers- (-1989)
ELECTRIC DISCHARGES
SUPERSONIC FLOW
RUNGE-KUTTA METHOD
CARBON DIOXIDE LASERS
DIFFERENTIAL EQUATIONS
FORTRAN
WIND TUNNELS
EQUATIONS
FLUID FLOW
GAS LASERS
ITERATIVE METHODS
LASERS
NUMERICAL SOLUTION
PROGRAMMING LANGUAGES
TUNNELS
420400* - Engineering- Heat Transfer & Fluid Flow
420300 - Engineering- Lasers- (-1989)