No. 522; Concluding paper on investigation of landing-gear drag carried out in N.A.C.A. 20-ft wind tunnel; tests of tail wheels and tail skids; drag of landing gear, for which interference between wheels and struts is small, is appreciably less with streamline wheels than with low-pressure wheels of equal load-carrying capacity. (Price 10¢) (See also - report n 518 1935 10 p. 10¢)
Drag of airplane wheels, wheel fairings and landing gears. II -- Nonretractable and partly retractable landing gears
Nat. Advisory Committee Aeronautics -- Report
1935
11 pages
Bibliography
Report
Englisch
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Engineering Index Backfile | 1935
|Drag of airplane wheels, wheel fairings, and landing gears
Engineering Index Backfile | 1934
|