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Model 309/319--Cessna participated in Boundary Layer Control (BLC) research from 1951 to 1955 with the U.S. Navy and Wichita University using a stock 170A modified to house a small gas turbine in the fuselage which blew air over the wing (1951). The 309A, first flown in February 1952, used an engine-driven electric generator to operate large fans in the wings to generate the air; the 309B of 1953 and 309C in 1954 used dry chemicals that generated airflow across the wings and flaps.
Cessna 309 family tree:
Cessna 309 company plan:
Another follow-on, the 319-A of 1953, had larger, more powerful flaps. With 225 hp Continental engine and BLC, the airplane had a stall speed of 32 mph. It could take off in 190 ft, land in 160 ft and make it in over a 50-ft obstacle in just 450 ft. As a research vehicle, the 309/319 was a success, but its commercial application was questionable--or as a Cessna test pilot wrote on a report after his first flight, "All in all, a rather nasty little monster!"
Cessna 319A in US Naval Research guise:
Technical depiction of Cessna 319A's BLC system:
See the various source documents in the attachments below.
Attachments
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092459 (319A).pdf2.7 MB · Views: 14
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017200 (309A, 309C, 319A).pdf5.4 MB · Views: 17
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015187 (309A, 309C, 319A).pdf3.3 MB · Views: 12
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012310 (309A, 309C, 319A).pdf1.5 MB · Views: 12
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010761 (309A and 319).pdf482.6 KB · Views: 11
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010750 (309A and 319).pdf485.6 KB · Views: 14
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006974 (309).pdf14.2 MB · Views: 14