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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)
Book Details
Author(s)Larry Wayne Mohn
ISBN / ASINB00072R8T2
ISBN-13978B00072R8T1
Sales Rank99,999,999
MarketplaceUnited States 🇺🇸
