Contribution of Wing Planform to Rolling Moment Derivative Due to Sideslip,(L Sub V) Sub W,at Subsonic Speeds. 80033

Contribution of Wing Planform to Rolling Moment Derivative Due to Sideslip,(L Sub V) Sub W,at Subsonic Speeds. 80033

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Product details

  • Loose-leaf
  • ESDU International PLC
  • United Kingdom
  • 0856793167
  • 9780856793165