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Transition and Drag Measurements on the Boulton Paul Sample of Laminar Flow Wing Construction
Contents: (Part 1) Measurements in the 13 ft x 19 ft Tunnel at the N.P.L. (Part 2) Measurements in the No. 2 11.5 ft. Tunnel at the R.A.E. (Part 3) Joint Discussion of Results, and Note.
Transition and Drag Measurements on the Boulton Paul Sample of Laminar Flow Wing Construction
Contents: (Part 1) Measurements in the 13 ft x 19 ft Tunnel at the N.P.L. (Part 2) Measurements in the No. 2 11.5 ft. Tunnel at the R.A.E. (Part 3) Joint Discussion of Results, and Note.
Transition and Drag Measurements on the Boulton Paul Sample of Laminar Flow Wing Construction
J. H. Preston (author) / N. Gregory (author) / K. W. Kimber (author)
1946
47 pages
Report
No indication
English
Aerodynamics , Aircraft , Laminar flow , Drag , Wings , United kingdom , Measurement , Construction , Ati-9619 , Ati collection , Foreign reports
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