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Calculation of the warp to produce a given load and the pressure due to a given thickness on thin slender wings in supersonic flow

Calculation of the warp to produce a given load and the pressure due to a given thickness on thin slender wings in supersonic flow - - London Her Majesty's Stationary Office 1965 - 36 p. - ARC R&M 3471 : 1965 .

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Universal Decimal Class. No.: DARC R&M 3471 : 1965

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