UNSTEADY AND QUASI-STEADY MODES OF THE FLOW OVER AN INTAKE TESTED IN A HOTSHOT WIND TUNNEL

Author:

Gounko Yu. P.,Kavun I. V.

Publisher

Pleiades Publishing Ltd

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference17 articles.

1. A. Pope and K. Goin, High-Speed Wind-Tunnel Testing (New York, 1965).

2. A. S. Korolev, B. V. Boshenyatov, I. G. Druker, and V. V. Zatoloka, Impulse Wind Tunnels in Aerodynamic Research (Nauka, Novosibirsk, 1978) [in Russian].

3. V. A. Zvegintsev, Short-Duration Gas-Dynamic Facilities. Part 1. Facilities for Academic Research (Parallel, Novosibirsk, 2014) [in Russian].

4. R. L. Williams, “Application of Pulse Facilities to Inlet Testing," J. Aircraft. 1 (10), 236–241 (1964); DOI: 10.2514/3.43589.

5. B. V. Boshenyatov, B. N. Gilyazetdinov, and V. V. Zatoloka, “Experimental Investigations of Hypersonic Intakes," in Aeromechanics: Collected Scientific Papers Devoted to the 60th Anniversary of Academician V. V. Struminskii (Nauka, Moscow, 1976), pp. 87–98 [in Russian].

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