Search Results for the EPA National Library Catalog

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Select Item	Title	Year Published
1	Applicability of First and Second Order Theory for the Determination of Subcritical Pressure Distributions on Non-Lifting Aerofoils.	1969
2	Lift Induced on a Swept Wing by a Two-Dimensional Partial-Span Deflected Jet at Mach Numbers from 0.20 to 1.30.	1971

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