Publisher
Springer Science and Business Media LLC
Subject
Aerospace Engineering,Transportation
Reference18 articles.
1. Wiggen, S., et al.: Motion-induced unsteady aerodynamic loads with development of vortical flow. J. Aircr. (2017).
https://doi.org/10.2514/1.C034308
2. Dobbs, S.K., Miller, G.D., Stevenson, J.R.: Self-induced oscillation wind tunnel test of a variable sweep wing. In: Structures, Structural Dynamics, and Materials and Co-located Conferences. American Institute of Aeronautics and Astronautics (1985)
3. Cunningham(Jr.), A.M., den Boer, R.G.: Overview of unsteady transonic wind tunnel test on a semispan straked delta wing oscillating in pitch. Final Report for Period March 1989–December 1993. 94-28128, Flight Dynamics Directorate Wright Laboratory an Air Force Materiel Command, Wright-Patterson Air Force Base, Ohio (1994)
4. Seshadri, S.N., Narayan, K.Y.: Shock-induced separated flows on the lee surface of delta wings. Aeronaut. J. 91, 128–141 (1987)
5. Miller, D.S., Wood, R.M.: Leeside flows over delta wings at supersonic speeds. J. Aircr. 21(9), 680–686 (1984)
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献