A TECHNIQUE TO MEASURE THE PRESSURE DISTRIBUTION ON THE SURFACE OF SPINNING WIND TUNNEL MODELS.
- Author
- MILLER MC
DA EDGEWOOD ARSENAL, ABERDEEN PROVING GROUND, MD. 21010 - Source
- IN: AERODYN. TEST. CONF. 9. PROC.; ARLINGTON, TEX.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 91-99; BIBL. 3 REF.
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- SOUFFLERIE PROFIL AERODYNAMIQUE MESURE DISTRIBUTION PRESSION COUCHE LIMITE DECOLLEMENT ECOULEMENT EFFET MAGNUS
- Keyword (en)
- WIND TUNNEL AEROFOIL MEASUREMENT PRESSURE DISTRIBUTION BOUNDARY LAYER FLOW SEPARATION MAGNUS EFFECT
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics
- Discipline
- Theoretical physics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL7730126674
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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