Abstract
The possible influence of fastening the models on a side pylon at their tests in wind tunnels on their aerodynamics at supersonic flow speeds has been considered. The physical problem of the pylon and the model interference has been investigated, and the estimates of the pylon influence on integral aerodynamic characteristics have been obtained. The numerical computations of the flow have been done using the averaged Navier-Stokes equations and the SST k-ω turbulence model in the range of freestream Mach numbers M = 2.5-5. As the investigation object the “classical” body of revolution of large aspect ratio is considered, which has a cruciform forward fins and six-blade tail stabilizers.
Similar content being viewed by others
References
Magnetic suspension of models in wind tunnels / composed by L. B. Belyaev and P. M. Shirmanov, Reviews of TsAGI, 1979, No. 557.
Simulation of the air-breathing engine at the investigations of flying vehicles in wind tunnels / composed by V. T. Zhdanov and P. I. Kurilkina, Reviews of TsAGI, 1972, No. 395.
Technique of the aerodynamic experiment at transonic speeds. Part II. Technique and method of testing the models with the imitation of jets of jet engines / composed by V. N. Kleev et al., Reviews of TsAGI, 1983, No. 622.
W. E. Dietz and M. C. Altstatt, Experimental investigation of support interference on an ogive cylinder at high incidence, AIAA Paper, 1978, P. 78–165.
L. E. Ericsson and J. P. Reding, Review of support interference in dynamic test, AIAA J., 1983, Vol. 21, No. 12, P. 1652–1666.
V. S. Zuenko, A. V. Lokotko, and A. A. Rafaelyanz, Technique of balance tests on a fin sting, in Proc. III. All-Union School on the Method of Aerophysical Research, Novosibirsk, 1982, P. 36–39.
M. Bikshapathi, N. Gopinath, and B. Venugopal, Effect of wind tunnel support systems on the aerodynamic characteristics of a fighter aircraft configuration, in Proc. 6th Symp. on Applied Aerodynamics and Design of Aerospace Vehicles. 21-23 November 2013, India. P. 25–29.
A. V. Lokotko, Improvement of accuracy of aerodynamic balance tests with regard for sting flow errors, Thermophysics and Aeromechanics, 1994, Vol. 1, No. 4, P. 355–359.
A. V. Lokotko, Implementation of the “doubling” method in aerodynamic experiment with suspension of the ducted models to the side pylon, in: Int. Conf. on the Methods of Aerophysical Research, June 30-July 6 2014, Novosibirsk, Russia, Abstracts, Part II, P. 128–129.
V. I. Kornilov, Three-dimensional Near-wall Turbulent Flows in Corner Configurations, Publishing House of SB RAS, Novosibirsk, 2013.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
About this article
Cite this article
Volkov, V.F., Mazhul, I.I. & Zvegintsev, V.I. Numerical simulation of the side pylon effect on the aerodynamic characteristics of models at their wind tunnel tests. Thermophys. Aeromech. 23, 319–328 (2016). https://doi.org/10.1134/S0869864316030021
Received:
Revised:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S0869864316030021