supported by the Fundamental Research Funds for the Central Universities (Nos. 3102019JC009 and G2016KY0002)
Civil aviation faces great challenges because of its robust projected future growth and potential adverse environmental effects. The classical Tube-And-Wing(TAW) configuration following the Cayley’s design principles...
supported by the Fundamental Research Funds for the Central Universities (Nos. 3102019JC009 and G2016KY0002)
Strong shock waves and flow separation often occur during the integration of nacelle and airframe for blended-wing-bodies with podded engines. To address this problem, this paper presents an integration method with nu...
Supported by the National Natural Science Foundation of China(51075203)
To evaluate the landing response of the large civil aircraft in the conceptual design phase , a method for simulating aircraft landing is given.The model for the shock absorber is investigated.The flexible airframe mo...