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" An airfoil is examined that has an upper surface shaped to control flow accelerations and pressure distribution over the upper surface and to prevent separation of the boundary layer due to shock wave formulation at high subsonic speeds well above the... "
Significant NASA Inventions - Page 34
by United States. National Aeronautics and Space Administration - 1973
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Scientific and Technical Aerospace Reports, Volume 14, Issues 13-16

Aeronautics - 1976
...US-Patent-Class-244-35R. US-Patent-Class-244-40R) Avail. US Patent Office CSCL OA An airfoil is examined that has an upper surface shaped to control flow accelerations...and pressure distribution over the upper surface and to prevent separation of the boundary layer due to shock wave formulation at high subsonic speeds well...
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NASA Patent Abstracts Bibliography

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office - Astronautics - 1978
...US-Patent-Class-244-35R: US-Patent-Class-244-40Ri Avail US Patent Office CSCL 01A An airfoil is examined that has an upper surface shaped to control flow accelerations...and pressure distribution over the upper surface and to prevent separation of the boundary layer due to shock wave formulation at high subsonic speeds well...
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