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- 54044252 contributor B1294031.
- 54044252 created "1951.".
- 54044252 date "1951".
- 54044252 date "1951.".
- 54044252 dateCopyrighted "1951.".
- 54044252 description "Bibliography: leaves 32-33.".
- 54044252 description "Thesis--California Institute of Technology.".
- 54044252 extent "iv, 118 l. (l. 37-118 mounted illus., diagrs.)".
- 54044252 issued "1951".
- 54044252 issued "1951.".
- 54044252 language "eng".
- 54044252 publisher "Pasadena,".
- 54044252 subject "Aerofoils.".
- 54044252 subject "Boundary layer.".
- 54044252 subject "Lift (Aerodynamics)".
- 54044252 subject "TL574.A4 D37".
- 54044252 subject "Trailing edge flaps.".
- 54044252 title "Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps.".
- 54044252 type "text".