Experimental investigation of temperature recovery factors on a 10 degree cone at angle of attack at a Mach number of 3.12

John R. Jack, Barry Moskowitz
Jul 1954

Temperature recovery factors on a thin-walled, metal, 10 degree included angle cone were obtained at a Mach number of 3.12 over a range of angles of attack from 0 to 10 degrees and for Reynolds numbers per foot from 1.5 X 10 (exp 6) to 8 X 10(exp 6).

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