A Correction Method for Cruising Fuel Consumption Characteristics Based on Circling Flight Test Data
A technology of flight test data and characteristics, applied in the aviation field, can solve problems such as the unique weight of the aircraft, the inability to obtain multiple sets of test flight data, and the inability to accurately measure the fuel consumption.
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[0050] A method for correcting cruise fuel consumption characteristics based on circling flight test data, characterized in that: comprising the following steps:
[0051] a. Select the altitude point, speed point and flight state. Under the same altitude, speed and aircraft weight, select n different roll angles (n is a variable, and the stable circling time is 3 to 5 minutes), and establish a stable circling. Hourly fuel consumption under different roll angles, the calculation formula is as follows:
[0052]
[0053] Among them, W px is the hourly fuel consumption, △W px is the fuel consumption of hovering, △T px is the circling time;
[0054] b. Correction of fuel consumption characteristics, including stable hovering mechanics model and engine mechanics model;
[0055] The equations of the stable hovering mechanics model are as follows:
[0056] L cosφ=G (2)
[0057] T=D(3)
[0058]
[0059]
[0060] CD=CD 0 +A·CL 2 (6)
[0061] Among them, L is the lift...
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