An experimental investigation of the effects of boundary layer suction on the performance of an aerothermopressor | ORKG Ask

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A theoretical and experimental investigation of the aerothermopressor process

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Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 /

Strike, W. T., author.
Pate, S., author.
ARO, Inc. sponsor.
United States. Air Force. Air Research and Development Command. sponsor.
Arnold Engineering Development Center. issuing body.

A second investigation was conducted in the 12in., intermittent, supersonic wind tunnel of the von K...

Investigation of boundary-layer suction on a 20-caliber Ogive cylinder at Mach numbers 2.5, 3.0, 3.5, and 4.0 /

Strike, W. T., author.
Pate, S., author.
ARO, Inc. sponsor.
United States. Air Force. Air Research and Development Command. sponsor.
Arnold Engineering Development Center. issuing body.

A second investigation was conducted in the 12in., intermittent, supersonic wind tunnel of the von K...