1. Hypersonic inviscid and viscous flow over a wedge and cone
2. 2Wells, W. and Armstrong, W.rTables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spherical bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data.NASATRR-127, 1961.
3. 4Peake, D. J. and Tobak, M.:Three-dimensional flows about simple components at angle of attack.AGARD LS-121,1982.
4. Basic experiment on a supersonic vortex flow around a missile body