Results of investigation of large chord wing model with duct to house simulated radiator suitable for liquid cooled engine; duct was expanded to reduce radiator losses, and installation of duct and radiator was made entirely within wing to reduce form and interference drag.
Investigation in 7- by 10-foot wind tunnel of ducts for cooling radiators within airplane wing
Nat Advisory Committee Aeronautics -- Report
1942
19 pages
Report
Englisch
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Wind-tunnel investigation of wing ducts on single-engine pursuit airplane
Engineering Index Backfile | 1943
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