Vol. 16, No. 1, 2024
Numerical Study of the Aerodynamics of the Head Unit during an Accident at the Start in Windy Conditions
p. 1 abstract
A High-Order Accuracy Method for Calculating the Initial Icing Stage of a Civil Aircraft’s Structural Elements
p. 13 abstract
Computation of the Evolution of Tollmien–Schlichting Waves Based on Global Stability Analysis
p. 29 abstract
Study of the Vortex-Resolving Method of the Throttling Effect on Pressure Pulsation Spectra in a Paired Supersonic Air Intake
p. 39 abstract
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
p. 50 abstract
Application of the Harmonic Balance Method to Calculate the First Booster Stage Tonal Noise
p. 63 abstract
Numerical Simulation of the Evolution of a Curved Turbulent Wake Subjected to an Adverse Pressure Gradient
p. 76 abstract
Numerical Study of the Features of the Propagation of Acoustic Disturbances in an Unregulated Supersonic Air Intake
p. 88 abstract
Application of Hybrid RANS/LES Methods for the Simulation of Shock-Induced Turbulent Boundary Layer Separation
p. 100 abstract
Automatic Block-Structured Grid Generation in Turbo Machine Blade Passages by TurboR&D.Mesher Software
p. 112 abstract
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
p. 123 abstract