S. V. Bobashev, Yu. P. Golovachov, N. P. Mende, P. A. Popov, B. I. Reznikov, V. A. Sakharov, A. A. Shmidt, A. S. Chernyshev, S. Z. Sapozhnikov, V. Yu. Mityakov, A. V. Mityakov, “Application of the gradient heat flux sensor to study pulsed processes in a shock tube”, Zhurnal Tekhnicheskoi Fiziki, 2008, Volume 78, Issue 12,Pages <nobr>103

This article is cited in 4 papers

Brief Communications

Application of the gradient heat flux sensor to study pulsed processes in a shock tube

S. V. Bobashev^a, Yu. P. Golovachov^a, N. P. Mende^a, P. A. Popov^a, B. I. Reznikov^a, V. A. Sakharov^a, A. A. Shmidt^a, A. S. Chernyshev^a, S. Z. Sapozhnikov^b, V. Yu. Mityakov^b, A. V. Mityakov^b

^a Ioffe Institute, St. Petersburg
^b St. Petersburg Polytechnic University

Abstract: The surface temperature of a model body of revolution placed in a pulsed supersonic nitrogen flow is measured with the help of a gradient heat flux sensor. From the measured temperature, a heat flux toward the surface of the body is determined. The steady flow of a viscous transcalent gas about the body is numerically calculated. The results of the numerical calculation and measuring data are in good agreement.

Received: 13.05.2008