主题：【原创】F-35B与中型航母的作战使用问题 -- 晨枫
家园 F35B 垂降时接入一5英尺直径风扇 难道不是相当一个涵道比变大了的发动机?
家园 这5英尺直径风扇的气流经过发动机吗？ 不经过！驱动这5英尺风扇的动力从哪里来？从发动机延长轴来。换句话说，发动机要增加出力，才能提供这额外的动力。机背辅助进气口确实提供额外进气，但这不是额外的冷却空气，而是流经发动机供发动机增加燃烧、增加出力的空气。
你还是认定喷气实际上是得到冷却的？
家园 这里 AM-2 Aluminum Matting- 复 这里
家园 看来AM2是试验过的 但关键还是在于：“F-35B喷气烧蚀甲板问题并不严重”这个说法的错误。
家园 AV-8B 用的 F-35B 也能用 如何能说
“F-35B喷气烧蚀甲板问题并不严重”这个说法的错误。The EAF and VTOL Pad AM-2 surfaces are representative of current US Marine Corps austere/forward deployed basing capabilities. These surfaces will be used to test F-35B compatibility during Short Takeoff (STO), Vertical Landing (VL), and Slow Landing (SL).家园 还是在回避 http://aviationweek.com/awin/us-navy-details-ship-mods-required-f-35
作为海军作战部长，格林纳特的话应该是靠谱的。这里也明确提到，LM和USMC早先提到F-35B和AV-8B的喷气温度相近是错误的说法：
The changes confirm that Lockheed Martin and the Marine Corps issued erroneous statements in early 2010 regarding the environmental effects of the F-35B’s exhaust. At that time, a company spokesman said that “extensive tests” had shown that “the difference between F-35B main-engine exhaust temperature and that of the AV-8B is very small, and is not anticipated to require any significant CONOPS changes for F-35B.”
你要是认为格林纳特和航空周刊的话不够权威，请举出更权威的数据。
- 复 还是在回避
家园 这些改动能确定跟温度有关? 天线，救生筏移位，等等这些多半还是跟"风变大了" 有关，并没直接证据"风变热了"。。。
现有的更温度有关的就是原有的简易机场用的铝制部件被拿来给F35B VERTICAL LANDING 时用了。。。"Certify"了
家园 你说与温度有没有关？ The changes confirm that Lockheed Martin and the Marine Corps issued erroneous statements in early 2010 regarding the environmental effects of the F-35B’s exhaust. At that time, a company spokesman said that “extensive tests” had shown that “the difference between F-35B main-engine exhaust temperature and that of the AV-8B is very small, and is not anticipated to require any significant CONOPS changes for F-35B.”