1. A comparative study of computational methods in cosmic gas dynamics;Albada;Astronomy and Astrophysics,1982
2. Bae, E.S., Gandhi, F., 2012. Upstream Active Gurney Flap for Rotorcraft Vibration Reduction, vol. 2, pp. 1354–1362.
3. Two-dimensional wind tunnel and computational investigation of a microtab modified airfoil;Baker;AIAA, Journal of Aircraft,2007
4. Barakos, G., Steijl, R., Badcock, K., Brocklehurst, A., 2005. Development of CFD capability for full helicopter engineering analysis. In: 31st European Rotorcraft Forum, 13–15 September, Florence, Italy, pp. 91.1–91.15.
5. Optimum two-per-revolution inputs for improved rotor performance;Cheng;AIAA, Journal of Aircraft,2005