Installation of an engine nacelle on a wing.
Great Britain.His Majesty's Stationery Office.
Aeronautical Research Council (Great Britain),issuing body.
November, 1939.
Part I. Model tests on a symmetrical wing -- part II. Underslung nacelles on cambered wings -- part III. Pitching-moment changes due to nacelles -- part IV. Effects of fuselage and tractor airscrew.