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

Name: Wing Lift Coefficient Increment at Zero Angle of Attack Due to Deployment of Plain Trailing-edge Flaps at Low Speeds. 97011
ISBN: 9781862460119

Publisher ESDU International PLC

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Book Details

PublisherESDU International PLC

ISBN / ASIN1862460116

ISBN-139781862460119

MarketplaceFrance 🇫🇷