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Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0. [Langley 8-ft transonic wind tunnel]

J. A. Penland, J. B. Hallissy, J. L. Dillon

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Key concepts: Aerodynamics, Airplane, Mach number, Delta wing, Wing, Hypersonic speed, Aerospace engineering, Aeronautics

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Aerodynamic characteristics of a hypersonic research airplane concept having a 70 deg swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0. [Langley 8-ft transonic wind tunnel] — Research Paper | ScholarLens