AN ANALYTICAL METHOD TO COMPUTE VISCOUS-INVISCID TRANSONIC FLOW ON AXISYMMETRIC AFTERBODIES INCLUDING JET EFFECTS AND BOATTAIL BLEED IN SEPARATED REGIONS.
- Author
- CALARESE W
AIR FORCE FLIGHT DYN. LAB., WRIGHT-PATTERSON AIR FORCE BASE, OHIO - Source
- IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1293; PP. 1-9; BIBL. 18 REF.
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- AVION ECOULEMENT TRANSSONIQUE ECOULEMENT CISAILLE INJECTION FLUIDE TRAINEE REDUCTION TRAINEE INTERACTION VISQUEUSE NON VISQUEUSE COUCHE LIMITE METHODE CALCUL DECOLLEMENT ECOULEMENT
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics
- Discipline
- Theoretical physics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL7630135006
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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