Wind Tunnel Test Results for a Canard Rotor/Wing Aircraft Configuration
Wind Tunnel Test Results for a Canard Rotor/Wing Aircraft Configuration
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- SKU # : 57-00166
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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 CompanyRecently Viewed Items
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Wind Tunnel Test Results for a Canard Rotor/Wing Aircraft Configuration
- Member Price :
- $15.00
- Your Price :
- $30.00
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