Wing Lift Coefficient Increment at Zero Angle of Attack Due to Deployment of Plain Trailing-edge Flaps at Low Speeds. 97011 Buy on Amazon

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Wing Lift Coefficient Increment at Zero Angle of Attack Due to Deployment of Plain Trailing-edge Flaps at Low Speeds. 97011

Book Details

ISBN / ASIN1862460116
ISBN-139781862460119
Sales Rank99,999,999
MarketplaceUnited States  🇺🇸
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