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

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Book Details

Author(s) Larry Wayne Mohn

Publisher For sale by the National Technical Information Service

ISBN / ASIN B00072R8T2

ISBN-13 978B00072R8T1

Sales Rank #99,999,999

Marketplace United States 🇺🇸