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#1
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I just compare P47D and fw190A8 at sea level. If we compare the data at 7000m altitude, P47D has more advantage because fw190a8 lose a lot of engine output there while P47D is still 2000-2300HP. Furthermore, the air density is only 1/2-1/3 of sea level, and aircrafts should maintain a longer time at high speed above Vmax. It's more easy to dive to a high Mach number where the 4-blade propeller has efficiency advantage. BTW, german broad chord 3-blade propeller loses 8% efficiency at Vmax compared with old 3-blade. Therefore, allied 4-blade prop should has more efficiency than german new wide blades. not 80% vs 80%, that's sth. 85% vs 75% at Vmax. Quote:
Last edited by BlackBerry; 06-06-2012 at 04:07 PM. |
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#2
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If you use Take Off Weights, the equilibrium speed of the FW-190 is higher than the P47. It does not matter though as neither aircraft can achieve equilibrium velocity as they are dynamic pressure and mach limited. The P47 always has higher limits. Quote:
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As such it is good approximation of Indicated Airspeeds and delivers a very good prediction of the performance trends you should see. |
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#3
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The 2300 hp for the R-2800 is at War Emergency Power and the 1980 hp for the BMW801D2 is at Erhohte Notleistung 1.58ata@2700U/min. |
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#4
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You guys need a weight and balance chart for the P47 series? |
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#5
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I'd be very interested in seeing one thanks
for the FW to clarify, is it 1,980 PS or 1,980hp? this has turned into a very interesting thread imo. Last edited by fruitbat; 06-06-2012 at 05:10 PM. |
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#6
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#7
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Thanks for posting the weight and balance chart
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#8
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p47D(R2800-59) 345mph=555km/@SL ,2300HP, and what 's the weight you want to use? Last edited by BlackBerry; 06-07-2012 at 01:41 AM. |
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