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On The Flow Over A Cone-cylinder Body At Mach Number One
Author(s): Yoshihara, Hideo
Corporate Author(s): Aircraft Laboratory, Wright Air Development Center
Date of Publication: 1952-01
Report number: WADC TR 52-295
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Effects Of The Upstream Influence Of A Shock wave At Supersonic Speeds In The Presence Of A Separated Boundary Layer
Author(s): Daniels, Lloyd E., Yoshihara, Hideo
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1954-01
Report number: WADC TR 54-31
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Unsteady Laminar Heat Transfer From A Flat Plate
Author(s): Yoshihara, Hideo
Corporate Author(s): Aircraft Laboratory
Date of Publication: 1955-10
Report number: WADC TR 55-370
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On The Flow Over A Finite Wedge In The Lower Transonic Region
Author(s): Yoshihara, Hideo
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-444

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