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Maximum Lift Coefficients for Aerofoil Sections at Mach Numbers from 0.60 to 0.75 - Amendment B

Part of the Aerodynamics series
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£150.00
Product Details
ESDU International PLC
1862464480 / 9781862464483
Loose-leaf
533.62
01/12/1954
United Kingdom
3 pages
210 x 300 mm
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