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 |