Abstract
Near-sonic inviscid gas flow in the working section of a wind tunnel with perforated walls is investigated in the context of the one-dimensional theory with Darcy's boundary condition.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
Literature cited
B. H. Goethert, Transonic Wind Tunnel Testing, Vol. 18, Pergamon Press, Oxford (1961).
Experimental Aerodynamics at Transonic Velocities, Part 1 (Survey of Foreign Literature 1969–1979) [in Russian], United Scientific and Technical Press Review, Central Aerohydrodynamic Institute, No. 599 (1981).
G. L. Grodzovskii, A. A. Nikol'skii, G. P. Svishchev, and G. I. Taganov, Supersonic Gas Flow Within Perforated Boundary Walls [in Russian], Mashinostroenie, Moscow (1967).
V. M. Neiland, “A new method of calculating transonic flows,” in: Sixth All-Union Congress on Theoretical and Applied Mechanics. Tashkent, 24–30 September 1986 (Abstracts of Proceedings) [in Russian], Tashkent (1986).
A. I. Ivanov, “Experimental investigation of gas flow near the perforated walls of a transonic wind tunnel,” Uch. Zap. TsAGI,18, 131 (1987).
Author information
Authors and Affiliations
Additional information
Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 143–148, November–December, 1988.
Rights and permissions
About this article
Cite this article
Neiland, V.M. One-dimensional transonic gas flow in a wind tunnel with perforated walls. Fluid Dyn 23, 920–924 (1988). https://doi.org/10.1007/BF01051830
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF01051830