Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Books Books
" 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 42
by United States. National Aeronautics and Space Administration - 1973
Full view - About this book

Scientific and Technical Aerospace Reports, Volume 14, Issues 13-16

Aeronautics - 1976 - 744 pages
...US-Patent-Class-244-35R. US-Patent-Class-244-40R) Avail. US Patent Office CSCL OÍA 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...
Full view - About this book

NASA Patent Abstracts Bibliography

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office - Astronautics - 1978 - 392 pages
...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...
Full view - About this book




  1. My library
  2. Help
  3. Advanced Book Search
  4. Download EPUB
  5. Download PDF