V. Mosharov

发表

Pressure sensitive paint for oscillating pressure fields measurements

C. Klein, V. Kulesh, S. Fonov, 1999, ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025).

Laboratory and marine study of photoluminescent sensors of oxygen dissolved in seawater

V. Mosharov, V. Radchenko, V. L. Vlasov, 2010 .

Laminar-turbulent flow over wedges mounted on sharp and blunt plates

V. Mosharov, V. Radchenko, V. Borovoy, 2009 .

Luminescent methods for investigating surface gas flows (Review)

V. Mosharov, 2009 .

Entropy-Layer Influence on Single-Fin and Double-Fin/Boundary-Layer Interactions

I. V. Struminskaya, I. Egorov, V. Mosharov, 2016 .

Pressure fields investigation by LPS technology on the aerospacecraft model

V. Mosharov, V. Radchenko, A. P. Bukov, 1994 .

Pyrometry using CCD cameras

V. Mosharov, V. Radchenko, I. Senyuev, 2013 .

Temperature sensitive paint application for investigation of boundary layer transition in short-duration wind tunnels

Volf Yakovlevich Borovoy, V. Mosharov, A. Noev, 2012 .

Laminar-turbulent flow around a wedge placed on sharp and blunted plates

V. Mosharov, V. Radchenko, A. Noev, 2012 .

Possibilities of the photoluminescence method for determining the oxygen concentration in the redox zone of the Black Sea in comparison with other methods

V. Mosharov, V. Radchenko, P. A. Stunzhas, 2013, Oceanology.

The two-component PSP investigation on a civil aircraft model in S2MA wind tunnel

Vladimir Evguenyevich Mosharov, M. Lyonnet, B. Deleglise, 1998 .

Study result for the application of two-component PSP technology to aerodynamic experiment

Vladimir Nikolaevich Radchenko, Vladimir Evguenyevich Mosharov, V. Pesetsky, 1998 .

Application of the PSP for Investigation of the Oscillating Pressure Fields

Vladimir Nikolaevich Radchenko, Rolf H. Engler, C. Klein, 1998 .

Set of luminescence pressure sensors for aerospace research

Vladimir Evguenyevich Mosharov, Vladimir Nikolaevich Radchenko, A. Orlov, 1993 .

Pressure sensitive paint application in shock wind tunnel

V. Mosharov, V. Radchenko, S. D. Phonov, 1995, ICIASF '95 Record. International Congress on Instrumentation in Aerospace Simulation Facilities.

VIDEOGRAMMETRY METHOD OF NON-CONTACT MEASUREMENTS OF INSTANTANEOUS DEFORMATION OF ROTATING PROPELLERS BLADES

Vladimir Petrovich Kulesh, Vladimir Nikolaevich Radchenko, Vladimir Evguenyevich Mosharov, 2013 .

Preliminary experimental results of heat flux surface field registration at the hypersonic aerodynamic shock tube using temperature sensitive paint

V. Mosharov, V. Radchenko, S. Surzhikov, 2018 .