Contribution of Fin and Tailplane to Sideforce and Yawing Moment Derivatives Due to Sideslip at Supersonic Speeds at Low Angle of Attack. 91031

Contribution of Fin and Tailplane to Sideforce and Yawing Moment Derivatives Due to Sideslip at Supersonic Speeds at Low Angle of Attack. 91031

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Product details

  • Loose-leaf
  • ESDU International PLC
  • United Kingdom
  • 0856797944
  • 9780856797941