Numerical Simulation For Supersonic Inlets
Numerical Simulation For Supersonic Inlets
- Neue Suche nach: Varner, M. O.
- Neue Suche nach: Martindale, W. R.
- Neue Suche nach: Phares, W. J.
- Neue Suche nach: Kneile, K. R.
- Neue Suche nach: Adams, J. C., Jr.
- Neue Suche nach: Varner, M. O.
- Neue Suche nach: Martindale, W. R.
- Neue Suche nach: Phares, W. J.
- Neue Suche nach: Kneile, K. R.
- Neue Suche nach: Adams, J. C., Jr.
Flows calculated for realistic engine-inlet conditions. Computer code LAPIN, large-perturbation inlet, developed to analyze large-perturbation, transient-flow fields in supersonic inlets. Robust, quick-running code capable of solving unsteady quasi-one-dimensional, inviscid-flow problems in mixed subsonic and supersonic regimes for inlets. Approach based upon quasi-one-dimensional, inviscid, unsteady formulation including engineering models of unstart/restart, bleed, bypass, and geometrical effects. Numerical solution of governing time-dependent equations of motion accomplished through shock-capturing, finite-difference algorithm. Program written in FORTRAN IV.
Dokumentinformationen
Numerical Simulation For Supersonic Inlets
NASA Tech Briefs ; 11 , 10
1987-11-01
Sonstige
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Englisch
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