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                             11 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 A High-Order Accuracy Method for Calculating the Initial Icing Stage of a Civil Aircraft’s Structural Elements Bosnyakov, S. M.

16 1 p. 13-28
artikel
2 Application of Hybrid RANS/LES Methods for the Simulation of Shock-Induced Turbulent Boundary Layer Separation Troshin, A. I.

16 1 p. 100-111
artikel
3 Application of the Harmonic Balance Method to Calculate the First Booster Stage Tonal Noise Rossikhin, A. A.

16 1 p. 63-75
artikel
4 Automatic Block-Structured Grid Generation in Turbo Machine Blade Passages by TurboR&D.Mesher Software Zagitov, R. A.

16 1 p. 112-122
artikel
5 Computation of the Evolution of Tollmien–Schlichting Waves Based on Global Stability Analysis Belyaev, K. V.

16 1 p. 29-38
artikel
6 Evaluation of the Accuracy of Modern Codes by Comparing the Calculated and Experimental Data on the Example of a Problem on a Supersonic Viscous Turbulent Gas Flow Around a Tandem of Back-Forcing and Forward-Forcing Steps Bosnyakov, S. M.

16 1 p. 123-155
artikel
7 Experimental Verification of the Method and Code for Calculating Low-Frequency Fluctuations at the Jet Boundary of a Full-Scale Subsonic Looped Type Wind Tunnel Bosnyakov, S. M.

16 1 p. 50-62
artikel
8 Numerical Simulation of the Evolution of a Curved Turbulent Wake Subjected to an Adverse Pressure Gradient Stabnikov, A. S.

16 1 p. 76-87
artikel
9 Numerical Study of the Aerodynamics of the Head Unit during an Accident at the Start in Windy Conditions Anikeeva, M. I.

16 1 p. 1-12
artikel
10 Numerical Study of the Features of the Propagation of Acoustic Disturbances in an Unregulated Supersonic Air Intake Shorstov, V. A.

16 1 p. 88-99
artikel
11 Study of the Vortex-Resolving Method of the Throttling Effect on Pressure Pulsation Spectra in a Paired Supersonic Air Intake Lyubimov, D. A.

16 1 p. 39-49
artikel
                             11 gevonden resultaten
 
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