Investigation at High and Low Subsonic Mach Numbers of Two Symmetrical 6-percent-thick Airfoil Sections Designed to Have High Maximum Lift Coefficients at Low Speeds

Investigation at High and Low Subsonic Mach Numbers of Two Symmetrical 6-percent-thick Airfoil Sections Designed to Have High Maximum Lift Coefficients at Low Speeds
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Total Pages : 37
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ISBN-10 : OCLC:1109673965
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Rating : 4/5 (65 Downloads)

Book Synopsis Investigation at High and Low Subsonic Mach Numbers of Two Symmetrical 6-percent-thick Airfoil Sections Designed to Have High Maximum Lift Coefficients at Low Speeds by : Nicholas J. Paradiso

Download or read book Investigation at High and Low Subsonic Mach Numbers of Two Symmetrical 6-percent-thick Airfoil Sections Designed to Have High Maximum Lift Coefficients at Low Speeds written by Nicholas J. Paradiso and published by . This book was released on 1952 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:


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