Method for obtaining thermal aerodynamic performance of flying aircraft
A technology of aerodynamic performance and acquisition method, which is applied in jet engine testing, gas turbine engine testing, etc., can solve the problems of huge calculation amount, large calculation amount of a single state, and low accuracy of combustion process simulation, and achieve high acquisition efficiency and acquisition method Simple and feasible, the effect of ensuring data accuracy
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[0037] The present invention will be described in detail below in conjunction with specific embodiments.
[0038] A method for obtaining the thermal performance of a flying aircraft provided by the present invention is suitable for flying aircraft, such as figure 1 shown. The flying vehicle includes a secondary aircraft 1 and a booster 4, the secondary aircraft 1 and the booster 4 are fixedly connected by an interstage connecting section 3, and the air control surface 5 is located at the tail of the booster 4. The secondary aircraft 1 and the tested engine 2 are designed by adopting the fusion design of the abdomen air intake scheme, and the secondary aircraft 1 meets the intake and exhaust requirements and equipment loading requirements of the tested engine 2. During the whole flying process, the rocket power is provided by the booster 4, and the flight attitude is controlled by the air control surface 5.
[0039] S1. Obtaining the thermal performance data of the flying veh...
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