歼10和FC-1的导弹寄生阻力数值与其他导弹（如aim120和aim9m）相同，重量也没有差很多，但是极速却比其他同挂载量飞机（如F-16C，F-2A，F-15E等）降低了二到三倍，而使用同款导弹的歼11b阻力要低得多，歼11b与其他战斗机的挂载阻力大致相同，而歼10和FC-1的挂载阻力过大，存在明显异常，导致这两款飞机在满挂载的时候比其他战斗机满挂载更慢了接近100km/h。根据视频：【战争雷霆】歼10的导弹挂架阻力是其他飞机的两倍_哔哩哔哩_bilibili
这种阻力存在于导弹而非挂架上，发射导弹可以让极速更快。应当减少这两款飞机的挂载阻力，并且可以酌情提高结构解体极速以适应更快的速度
为防止“挂载阻力对大推力飞机的影响比小推力飞机的影响小”的说法，我应当说明，我使用f15e举例是因为它可以使用6+2挂载，我需要补充的是，f16c和f2a作为和歼10体型和发动机比较相似的飞机，它们使用6导弹挂载时极速减小的幅度仍是歼10的1/3左右（约减小34km/h极速），而阵风战斗机挂载8发导弹时速度损失较多是因为阵风机体阻力极小，对挂载阻力敏感导致的，不应作为参考
ISSUE区管理员驳回了我的ISSUE，理由是不同飞机之间没有可对比性，但是我认为“对比”这个行为本身正是因为“不同”才得以存在，如果用相同的飞机，何来对比？所以我来到了论坛，不知论坛管理员可否回答或提交给开发组。翻译为英语
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The parasitic drag values of missiles on the J-10 and FC-1 are the same as those of other missiles (such as the AIM-120 and AIM-9M), and their weights are not significantly different. However, the reduction in maximum speed is two to three times greater than that of other aircraft with the same payload (such as the F-16C, F-2A, and F-15E). In contrast, the J-11B, which uses the same type of missiles, has much lower drag. The J-11B’s payload drag is roughly the same as that of other fighter jets, while the J-10 and FC-1 exhibit abnormally high payload drag. This anomaly causes these two aircraft to be nearly 100 km/h slower than other fighters when fully loaded. According to the video (【战争雷霆】歼10的导弹挂架阻力是其他飞机的两倍_哔哩哔哩_bilibili), this drag originates from the missiles rather than the pylons, and launching the missiles results in a higher maximum speed. It is recommended to reduce the payload drag of these two aircraft and, where appropriate, increase their structural limit speed to accommodate faster velocities.
To address the argument that “the impact of payload drag on high-thrust aircraft is smaller than on low-thrust ones,” I should clarify that I used the F-15E as an example because it can carry a 6+2 payload configuration. What I need to add is that for the F-16C and F-2A—aircraft with a size and engine performance comparable to the J-10—when they carry 6 missiles, the reduction in their maximum speed is still only about 1/3 of that of the J-10 (approximately a 34 km/h decrease). As for the Rafale fighter jet, its relatively significant speed loss when carrying 8 missiles is due to its extremely low airframe drag, making it sensitive to payload-induced drag. Thus, it should not be used as a reference.
The administrator in the ISSUE section rejected my issue on the grounds that there is no comparability between different aircraft. However, I believe that “comparison” itself exists precisely because of “differences”—if the aircraft were identical, there would be no need for comparison at all. Therefore, I have come to the forum and wonder if the forum administrator can respond to this or submit it to the development team.
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支持
F2的导弹甚至要更加重
complete sentence
agree
比较一定要找有不同的来比较 🖐🏻😭🖐🏻