Wing Lift Coefficient Increment at Zero Angle of Attack Due to Deployment of Trailing-edge Split Flaps at Low Speeds. 97009
📄 Viewing lite version
Full site ›
⌛ 🇫🇷 France pricing being fetched…
Prices will appear once fetched — usually within a few minutes.
View in:
🇺🇸 USA
Book Details
PublisherESDU International PLC
ISBN / ASIN1862460132
ISBN-139781862460133
MarketplaceFrance 🇫🇷