Supersonic flow over paired compression wedges of different sweep installed on the pre-compression surface

Author:

Gounko Yu. P.,Mazhul I. I.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Reference15 articles.

1. S.M. Bosnyakov, A.N. Minailos, and N.Kh. Remeev, Investigation of three-dimensional supersonic gas flow around two-step wedges of finite width, Uch. zapiski TsAGI, 1980, Vol. 11, No. 1, P. 96–101.

2. S.M. Bosnyakov and N.Kh. Remeev, Investigation of three-dimensional supersonic gas flow around a wedge of finite width under angles of attack and yaw, Uch. zapiski TsAGI, 1981, Vol. 12, No. 6, P. 16–24.

3. S.M. Bosnyakov and N.A. Zlenko, Computation of coefficients of the flow three-dimensionality near the surfaces of wedges of finite width, Trudy TsAGI, 1983, No. 2187, P. 15–23.

4. S.M. Bosnyakov and N.A. Zlenko, Approximate calculation of three-dimensionality coefficients for a supersonic inviscid gas flow around two-step compression wedges of finite width, Trudy TsAGI, 1985, No. 2284, P. 3–10.

5. S.M. Bosnyakov and N.Kh. Remeev, Investigation of three-dimensional supersonic gas flow around a twodimensional air intake with side cheeks, Uch. zapiski TsAGI, 1980, No. 5, P. 40–46.

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