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Flight Testing at Edwards AFB in the 1950s

机译:1950年代在爱德华兹空军基地进行的飞行测试

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摘要

The high-performance MIG-15 over Korea in the early 1950s spurred development of a new US fighter. The USAF wanted supersonic speeds and 50,000 foot altitude capability. North American designed their Mach 1.2 F-100 utilizing Pratt &Whitney's new 10,000-pound thrust engine, the J57, to meet the USAF desires. In those early days of high performance jets, with an industry having only rudimentary knowledge of supersonic aerodynamics, no computers to help design either airframes or engines, and a wing sweepback design copied from a German jet, it was no surprise that the airframe had very troubling flight characteristics (highlighted when NA's chief test pilot George Welch was killed during a high-speed dive, the first of several crashes), and the engine encountered severe compressor stalls caused by inlet duct curvature. Both NA and P&W expanded their flight test operations to rectify their individual problems.
机译:1950年代初,高性能的MIG-15在朝鲜上空,刺激了新型美国战斗机的研制。美国空军需要超音速和50,000英尺的高度能力。北美公司使用普惠公司的新型10,000磅推力发动机J57设计了其Mach 1.2 F-100,以满足美国空军的需求。在高性能喷气机的早期,一个行业仅对超音速空气动力学有基本的了解,没有计算机可以帮助设计机身或发动机,并且没有仿制德国喷气机的机翼后掠设计,因此机身具有令人不安的飞行特性(当北美航空的首席试飞员乔治·韦尔奇在高速潜水中遇难时丧生,这是几次坠机事故中的第一起),并且发动机因进气道弯曲而导致压缩机严重失速。 NA和P&W都扩大了飞行测试业务,以纠正各自的问题。

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  • 来源
    《Cockpit》 |2013年第julaadeca期|43-46|共4页
  • 作者

    Harry P. Schmidt;

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