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Investigation of Flow Separation on a Two-Dimensional Flat Plate Having a Variable-Span Trailing-Edge Flap at M = 3 and 5
Author(s): Pate, S. R.Corporate Author(s): ARO, Inc.
Date of Publication: 1964-03
Report number: AEDC TDR 64-14
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Investigation of Boundary-Layer Transition on Swept Wings at Mach Numbers 2.5 to 5
Author(s): Pate, S. R., Brillhart, R. E.Corporate Author(s): ARO, Inc.
Date of Publication: 1963-07
Report number: AEDC TDR 63-109
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