Pièce 21 - 'A Numerical Method of Determining Subsonic Compressible Flow Past an Obstacle. II Joukowski Aerofoil'. Division of Aeronautics, Aerodynamics Note No 61 by G K Batchelor

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Cote

BACH/B/1/21

Titre

'A Numerical Method of Determining Subsonic Compressible Flow Past an Obstacle. II Joukowski Aerofoil'. Division of Aeronautics, Aerodynamics Note No 61 by G K Batchelor

Date(s)

  • Dec 1944 (Production)

Niveau de description

Pièce

Étendue matérielle et support

1 doc

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