Aeroplane and Commercial Aviation News, 83. kötet1952 |
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14. oldal
... wing planforms . The author is an authority on this subject and was responsible for the aerodynamics of the Douglas Skyray . 1000 M.PM 12 10 08 06 04 .02 STABILITY +. Straight , Swept ALTHOUGH every aerodynamicist insists that wing ...
... wing planforms . The author is an authority on this subject and was responsible for the aerodynamics of the Douglas Skyray . 1000 M.PM 12 10 08 06 04 .02 STABILITY +. Straight , Swept ALTHOUGH every aerodynamicist insists that wing ...
16. oldal
... wing and the swept wing , but the percentage airfoil thickness in the direction of flight is thinner for the swept wing . For the delta wing this same ratio is obtained if the wing - root thickness is approximately 5 per cent . It ...
... wing and the swept wing , but the percentage airfoil thickness in the direction of flight is thinner for the swept wing . For the delta wing this same ratio is obtained if the wing - root thickness is approximately 5 per cent . It ...
18. oldal
... wing aeroplane is somewhat lower than that of the straight - wing aeroplane at low Mach numbers ; it increases at low - supersonic Mach numbers and then decreases gradually with Mach number . Here , again , the maximum values are ...
... wing aeroplane is somewhat lower than that of the straight - wing aeroplane at low Mach numbers ; it increases at low - supersonic Mach numbers and then decreases gradually with Mach number . Here , again , the maximum values are ...
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Maillard E F 648 | 2 |
C S Magnificent | 3 |
Park Sir Keith 485 | 5 |
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