Model tests definitely showed that conventional NACA 23,000 airfoil series wing was superior in practically all respects to laminar flow wing; development of "butterfly" tail; landing gear selection; selection of engine simmered down to Continental model, due to slight cost and initial delivery advantage; each major component designed, built and tested to destruction; performance data listed.
Development of beech bonanza light four-place high performance airplane
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 55 , n 7
1947
4 pages
Article (Journal)
English
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“DEVELOPMENT OF THE BEECH BONANZA LIGHT FOUR-PLACE HIGH PERFORMANCE AIRPLANE”
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