An experimental investigation at a Mach number of 4.95 of flow in the vicinity of a 90 degree interior corner alined with the free-stream velocity, by P. Calvin Stainback et al.

Title:	An experimental investigation at a Mach number of 4.95 of flow in the vicinity of a 90 degree interior corner alined with the free-stream velocity
Author:	Stainback, P. Calvin
Author:	Langley Research Center
Note:	National Aeronautics and Space Administration, 1960

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Subject:	Aerodynamic interference
Subject:	Boundary layer flow
Subject:	Corner flow
Subject:	Free flow
Subject:	Hypersonic heat transfer
Subject:	Laminar flow
Subject:	Mach number
Subject:	Reynolds number
Subject:	Shock layers
Subject:	Stagnation temperature
Subject:	Static pressure
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