Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps.
Published: 1951
Place of publication: Pasadena
Language: eng
Number of pages: 118
Subjects: Aerofoils.; Lift (Aerodynamics); Boundary layer.; Trailing edge flaps.
Notes: Bibliography: leaves 32-33.
Thesis--California Institute of Technology.
On cover: Guggenheim Aeronautical Laboratory, California Institute of Technology.