Abstract
Disturbance propagation in laminar boundary layers is investigated at large freestream velocities. An integral relation determining the disturbance propagation velocity in the weak hypersonic interaction regime is obtained for the first time.
Similar content being viewed by others
References
Yu. D. Shevelev, Three-Dimensional Problems of Theory of Laminar Boundary Layers [in Russian] (Nauka, Moscow, 1977).
V. I. Shalaev, Application of Analytical Methods in theModern Aeromechanics. Part 1. Boundary Layer Theory [in Russian] (Moscow Institute of Sciences and Technology, 2011).
I. I. Lipatov, “Disturbance Propagation in Supersonic Boundary Layers,” FluidMechanics and Its Application 35, 369 (1996).
R. Krechetnikov and I. I. Lipatov, “On Upstream Influence in Supersonic Flows,” J. Fluid Mech. 539, 167 (2005).
Author information
Authors and Affiliations
Corresponding author
Additional information
Original Russian Text © I.I. Lipatov, Q.N. Ngo, 2018, published in Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, 2018, No. 4, pp. 90–94.
Rights and permissions
About this article
Cite this article
Lipatov, I.I., Ngo, Q.N. Disturbance Propagation in Boundary Layers under the Conditions of Weak Hypersonic Interaction. Fluid Dyn 53, 531–535 (2018). https://doi.org/10.1134/S0015462818040080
Received:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S0015462818040080