1. Aircraft response in an airfield arrestor system during an overrun;Heymsfield;J Transp Eng,2012
2. Pashilkar A, Ismail S, Ayyagari R, Sundararajan N. Design of a nonlinear dynamic inversion controller for trajectory following and maneuvering for fixed wing aircraft. 2013 IEEE symposium on computational intelligence for security and defense applications (CISDA); 2013 Apr 16–19; Piscataway, NJ: IEEE Press; 2013. p. 64–71.
3. Air intake design for the acceleration propulsion unit of the LAPCAT-MR2 hypersonic aircraft;Meerts,2013
4. Williams JG, Steenken WG, Yuhas AJ. Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows. Edwards (CA): Dryden Flight Research Center; 1996 Sep. Report No.: NASA-CR-198052.
5. Kopasakis G, Connolly JW, Seidel J. Propulsion system dynamic modeling of the NASA supersonic concept vehicle for AeroPropulsoServoElasticity. Reston: AIAA; 2014. Report No.: AIAA-2014-3684.