Aeroplane and Commercial Aviation News, 90. kötet1956 |
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1 - 3 találat összesen 71 találatból.
17. oldal
... wing area and approximately the same take - off and landing weight . Equivalent flat - plate area ( sq . ft . ) Weight left for fuel ( lb. ) Take - off power loading ( lb./b.h.p . ) Wing loading ( lb./sq . ft . ) Distance to clear 50 ft ...
... wing area and approximately the same take - off and landing weight . Equivalent flat - plate area ( sq . ft . ) Weight left for fuel ( lb. ) Take - off power loading ( lb./b.h.p . ) Wing loading ( lb./sq . ft . ) Distance to clear 50 ft ...
18. oldal
... WING STRUT C1 = 1-2 CL = 0 · 77 PROFILE DRAG COEFFICIENT ( WING WITH STRUT ) 0.015 0.010 0.005 · 4-85X STRUT THICKNESS = EQUIVALENT STRUT LENGTH ADDITIONAL DRAG IN THE REGION OF THE JOIN 0.6 0.4 0.2 DUE TO STRUT WING WITHOUT STRUT 0.4 ...
... WING STRUT C1 = 1-2 CL = 0 · 77 PROFILE DRAG COEFFICIENT ( WING WITH STRUT ) 0.015 0.010 0.005 · 4-85X STRUT THICKNESS = EQUIVALENT STRUT LENGTH ADDITIONAL DRAG IN THE REGION OF THE JOIN 0.6 0.4 0.2 DUE TO STRUT WING WITHOUT STRUT 0.4 ...
26. oldal
... wing of the same aspect ratio under cruising conditions . The aspect ratio is smaller than for ordinary wings , so that the annular wing is really worse off than it seems . To make up for the resulting large induced drag the coleopter ...
... wing of the same aspect ratio under cruising conditions . The aspect ratio is smaller than for ordinary wings , so that the annular wing is really worse off than it seems . To make up for the resulting large induced drag the coleopter ...
Tartalomjegyzék
Miles Thomas will be appointed by the Minister Before passing | 16 |
MATTERS OF MOMENT | 18 |
B E A Plans for 1956 | 4 |
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