1. Second-order compressible boundary-layer theory with application to blunt bodies in hypersonic flow;Van Dyke,1962
2. Higher-order boundary-layer theory;Gersten,1976
3. The effect of Prandtl number on second-order heat transfer;Gersten,1974
4. K. Gersten, Effect of Prandtl number on second-order heat transfer at an axisymmetric stagnation point, to be published.
5. Higher approximations in boundary-layer theory. Part I: general analysis;Van Dyke;J. Fluid Mech.,1962