1. Die Grenzschicht an der ebenen Platte mit Absaugen und Ausblasen;SCHLICHTING;Luftfahrtf.,1942
2. A. GRIFFITH and F. MEREDITH. The possible improvement in aircraft performance due to the use of boundary layer suction. R.A.E., Rep. No. E 3501 (A.R.C 23/5).
3. Note on the velocity and temperature distributions attained with suction on a flat plate of infinite extent in compressible flow;YOUNG;Quart. J. Mech. Appl. Math.,1948
4. On the laminar compressible boundary layer over a flat plate with suction or injection;LEW;J. Aero. Sci.,1955
5. Asymptotische Absaugegrenzschichten an längsangeströmten zylindrischen Körpern;WUEST;Ing. Archiv.,1955