本文讨论空-空导弹和机炮排气尾流冲刷加热对 F-14“雄猫”(Tomcat)战斗机结构预期的和实际的影响。“响尾蛇”导弹、“麻雀”导弹以及“维根”(Vulcan)多管机炮的排气尾流,对关键构件的热影响特别引人注目。本研究一开始力求估计出影响的区域和解决问题的若干途径。更为重要的是本文探索了试验后修改设计的过程。提出了飞机主要构件受“响尾蛇”和“麻雀”导弹以及“维根”机炮尾流影响的分析估计和实际测到的热响应。此外,本文还叙述了地面和空中发射试验的结构加热影响问题(包括测试设备)以及对受尾流冲刷构件的维护经验。 This article discusses the expected and practical impact of air-to-air missiles and cannon exhaust wake fouling on the structure of the F-14 Tomcat fighter aircraft. The thermal effects on key components are particularly noticeable with the tail vortex of the Rattlesnake, Sparrow and Vulcan multi-barrel guns. In the beginning, the study sought to estimate the areas affected and ways to solve the problem. More importantly, this article explores the process of modifying a design after testing. The main components of the aircraft are analyzed and estimated by the wake influence of the “Rattlesnake” and “Sparrow” missiles and the “Wigan” cannon and the actually measured thermal response. In addition, this article describes the structural heating effects of ground and air launch tests (including test equipment) as well as maintenance experience with wake wash components.