1. Presented as Preprint 64-4 at the AIAA Aerospace Sciences Meeting, New York, January20-22,1964; revision received July 13, 1964. The work discussed in this paper was carried out under the sponsorship and with the financial support of U. S. Air Force, Grant No. AF-AFOSR-54-63. This paper supercedes Graduate Aeronautical Laboratory, California Institute of Technology, Separated Flows Project Technical Report 3 (October 4, 1963).
2. Zur Berechnung der Grenzschichten
3. On the Boundary-Layer Equations in Hypersonic Flow and Their Approximate Solutions