Tests to determine aerodynamic characteristics of semi-span tail surface of fighter type airplane were carried to maximum Mach number of 0.7 except for model configurations for which maximum allowable loads were reached at lower speeds; results show effects of elevator nose shape, elevator trailing edge angle, and trailing edge strips.
Tests of full-scale horizontal tail surface in Langley 16-foot high-speed tunnel
Nat Advisory Committee Aeronautics -- Tech Note
1946
24 pages
Supp sheets, Bibliography
Report
Englisch
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Aerodynamic tests of full-scale TBF-1 Aileron installation in Langley 16-foot high-speed tunnel
Engineering Index Backfile | 1944
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