1. HoffmanN. R.SpielbergI. N. “Subsonic Flutter Tests of an Unswept All-Moveable Tail,” Wright Air Development Center WADC-TR-54-53, Wright-Patterson AFB, Dayton, OH, 1954.
2. CooleyD. E. “Subsonic Flutter Model Tests of a Low Aspect Ratio Unswept All-Moveable Tail,” Wright Air Development Center WADC-TR-58-31, Wright-Patterson AFB, Dayton, OH, 1958.
3. “Department of Defense Joint Service Specification Guide—Aircraft Structures,” JSSG-2006, 30 Oct. 1998.
4. RoskamJ., Airplane Design Part IV: Layout Design of Landing Gear and Systems, Roskam Aviation and Engineering Copdrp., Ottawa, KS, 1989, pp. 236–237.
5. GrahamD.McRuerD. T., Analysis of Nonlinear Control Systems, Wiley, New York, 1961, pp. 77–143.