Transition and drag measurements on the Boulton Paul sample of Laminar-flow wing construction.
Great Britain.His Majesty's Stationery Office.
Great Britain.Aeronautical Research Committee,issuing body.
"November, 1946".
Part I measurements in the 13 by 9 feet tunnel at the N.P.L. -- part II measurements in the No. 2, 11 1/2 feet tunnel at the R.A.E. -- part III discussion of results and note.