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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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