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Wind Tunnel Test Results for a Canard Rotor/Wing Aircraft Configuration

Wind Tunnel Test Results for a Canard Rotor/Wing Aircraft Configuration

  • Presented at Forum 57
  • 13 pages
  • SKU # : 57-00166

  • Your Price : $30.00

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Wind Tunnel Test Results for a Canard Rotor/Wing Aircraft Configuration

Authors / Details: Thomas L. Thompson, The Boeing Company; Roger L. Smith, The Boeing Company; Moutaz Helwani, The Boeing Company; Gerald A. Shockey, The Boeing Company; Scott L. Schwimley, The Boeing Company