Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method (NASA contractor report)

Name: Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method (NASA contractor report)
Author: Larry Wayne Mohn
ISBN: 978B00072R8T1

Author Larry Wayne Mohn

Publisher For sale by the National Technical Information Service

📄 Viewing lite version Full site ›

🌎 Shop on Amazon — choose country

🇺🇸 USA 🇨🇦 Canada 🇬🇧 UK 🇩🇪 Germany 🇫🇷 France 🇮🇳 India

Price not listed

🛒 Buy New on Amazon 🇺🇸

Book Details

Author(s)Larry Wayne Mohn

PublisherFor sale by the National Technical Information Service

ISBN / ASINB00072R8T2

ISBN-13978B00072R8T1

Sales Rank99,999,999

MarketplaceUnited States 🇺🇸