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2. Gilev, V. M. and Kozlov, V. V.: Excitation of Tollmien-Schlichting Waves in the Boundary Layer on a Vibrating Surface. J. Applied Mech. and Tech. Phys., Vol. 25, No. 6, November/December 1984, pp. 874 – 877.
3. Pilipenko, A. A. and Shapovalov, G. K.: Effect on Model Vibration on Transition form Laminar to Turbulent Boundary Layer Flow. Fluid Mechanics - Soviet Research, Vol. 17, No. 4, July- August 1988, pp. 68 – 76.
4. Final Report on LFC Aircraft Design Data Laminar Flow Control Demonstration Program. NOR 67–136 (Contract AF 33(657)–13930), Northrop Corp., June 1967.
5. Kendall, J. M.: Wind-Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition. Presented at the 12th Aerospace Sciences Meeting, Washington, DC, January 1974, AIAA Paper No. 74–133.