1. A. Jameson and W. Schmidt, Numerical solutions of the Euler equations by finite volume methods using Runge–Kutta time-stepping schemes. AIAA Paper No. 81–1259, AIAA 14th Fluid and Plasma Dynamics Conf., Palo Alto, CA, 23–25 June 1981.
2. Transonic flow calculations for aircraft. Lecture Notes in Mathematics;Jameson,1985
3. A vertex based multigrid algorithm for three-dimensional compressible flow calculations;Jameson,1986
4. W. K. Anderson and J. L. Thomas, A comparison of finite volume flux vector splittings for the Euler equations. AIAA Paper No. 85–0122, AIAA 23rd Aerospace Science Meeting, Reno, NV, 14–17 January 1985.
5. R. W. Newsome, A comparison of Euler and Navier–Stokes solutions for supersonic flow over a conical delta wing. AIAA Paper No. 85–0111. AIAA 23rd Aerospace Science Meeting, Reno, NV, 14–17 January 1985.