典型文献
Virtual flight test techniques to predict a blended-wing-body aircraft in-flight departure characteristics
文献摘要：
As one of the promising configurations of the next generation of commercial aircraft,research on departure characteristics of the Blended-Wing-Body(BWB)is of great signification to safe flight limits.A three-degree-of-freedom(3-DOF)virtual flight test in a wind tunnel has been implemented for a candidate configuration to predict the departure characteristics.The support mechanism,the test model and the control law of the virtual flight test are introduced.In order to show the relationship between virtual flight test and actual flight test,the similarity criterion is also given.In open loop,the model has mild oscillations in the longitudinal and lateral directions,which are stable in closed-loop.The effect of flight control has been verified in virtual flight and actual subscale flight test.The analysis of system identification results indicate that the model has a good response to the excitation signal,and the response is in reasonable agreement with the flight test.Finally,the virtual flight departure test results are compared with the flight test.It shows that there is a good correspondence between the angle of attack and the elevator deflection at departure.This gives promising evidence of the practicability of virtual flight testing to predict departure of a BWB.
文献关键词：
中图分类号：
作者姓名：
Junquan FU;Zhiwei SHI;Zheng GONG;Mark H.LOWENBERG;Dawei WU;Lijun PAN
作者机构：
Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;University of Bristol,Bristol BS8 1TR,United Kingdom;COMAC Shanghai Aircraft Design and Research Institute,Shanghai 201210,China
文献出处：
引用格式：
[1]Junquan FU;Zhiwei SHI;Zheng GONG;Mark H.LOWENBERG;Dawei WU;Lijun PAN-.Virtual flight test techniques to predict a blended-wing-body aircraft in-flight departure characteristics)[J].中国航空学报（英文版）,2022(01):215-225
A类：
signification
B类：
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AB值：
0.503857
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