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Wing Lift Coefficient Increment at Zero Angle of Attack Due to Deployment of Trailing-edge Split Flaps at Low Speeds. 97009

Name: Wing Lift Coefficient Increment at Zero Angle of Attack Due to Deployment of Trailing-edge Split Flaps at Low Speeds. 97009
Author: Unknown
ISBN: 9781862460133

PublisherESDU International PLC

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Book Details

PublisherESDU International PLC

ISBN / ASIN1862460132

ISBN-139781862460133

MarketplaceFrance 🇫🇷