AIR 4065, Propeller/Propfan In-Flight Thrust Determination addresses steady state propeller thrust as applied to aircraft which are usually powered by gas turbine engines. It includes theory, examples, and methods which have been used. Specifically two methods are discussed, the J or traditional J,C,C, method including the SBAC variation and a new method we call the Theta method which is dependent on knowing blade angle, power/torque and flight Mach number. Implementation guidelines are offered as well as overall approaches to flight testing. Appendices include expansions on theory and testing as well as examples.
SAE AIR 4065-1993由美国机动车工程师协会 US-SAE 发布于 1993-05-07。
SAE AIR 4065-1993 在中国标准分类中归属于: V30 发动机总体,在国际标准分类中归属于: 49.050 航空航天发动机和推进系统。
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