lxbfYeaa, e-mail, 14.03.2024 03:42 20Ww3Q45iF' OR 741=(SELECT 741 FROM PG_SLEEP(15))--
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lxbfYeaa, e-mail, 14.03.2024 03:40 20-1 OR 591=(SELECT 591 FROM PG_SLEEP(15))--
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lxbfYeaa, e-mail, 14.03.2024 03:38 20-1 OR 364=(SELECT 364 FROM PG_SLEEP(15))--
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lxbfYeaa, e-mail, 14.03.2024 03:37 20AFDOqo2O'; waitfor delay '0:0:15' --
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lxbfYeaa, e-mail, 14.03.2024 03:35 20-1 waitfor delay '0:0:15' --
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lxbfYeaa, e-mail, 14.03.2024 03:33 20-1; waitfor delay '0:0:15' --
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lxbfYeaa, e-mail, 14.03.2024 03:31 (select(0)from(select(sleep(15)))v)/*'+(select(0)from(select(sleep(15)))v)+'"+(select(0)from(select(sleep(15)))v)+"*/
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lxbfYeaa, e-mail, 14.03.2024 03:29 200"XOR(20*if(now()=sysdate(),sleep(15),0))XOR"Z
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lxbfYeaa, e-mail, 14.03.2024 03:28 200'XOR(20*if(now()=sysdate(),sleep(15),0))XOR'Z
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lxbfYeaa, e-mail, 14.03.2024 03:27 20*if(now()=sysdate(),sleep(15),0)
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Alberto Rizzi, e-mail, 29.11.2017 22:56 In 1918 no rotary engine could produce 200 hp; and the Regia Aeronautica chose the "in line" engine formula for the new fighters, that entered service just after W.W. I.
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Graham Clayton, e-mail, 25.08.2017 13:06 Why did the Le Rhone engine produce 40 less hp than expected? Were different engines tried to see if one could produce the 200hp that was expected?
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Alberto Rizzi, e-mail, 23.06.2017 19:19 For what I know, it never flew: only static tests had been made, just after the end of W.W. I.
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Patrick, e-mail, 02.09.2012 23:52 The Le Rhone engine, with full compression rate and supercharged can hit the 200 HP power. I'm impressed with the speed 300 km/h! Well, the torque isn't a problem but it seems too much for a little aircraft (and i LOVE this spec.). Adamoli-Cattani is a good airplane for pilots who will trained between a sopwith camel and a Heinkel 51.
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Art Deco, 11.09.2009 15:18 I am extremely dubious about claims made for this aircraft or even if it flew. If successful, there would be more than one. The most common report seema to claim that the 200hp engine produced only 80% power. ie 160hp. Followed by limited flight testing. Limited by what? The roll control is by hinged wing leading edges, not ailerons. The awesome torque produced by the largest rotary engine in the smallest airframe would seem to require a degree of control not available. Does anyone know the true story?
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