In this paper, the large-eddy method and the Schnerr鈥揝auer cavitation model are combined to simulate a NACA0009 hydrofoil near the free surface. The numerical method used is validated by comparing the characteristics of TLV cavitation with available experimental data. The results show that the ...
To emphasizes the importance of experimental data in validating computational models and provides valuable insights into the aerodynamic characteristics of symmetrical air foil sections. The results of the study can be useful for engineers and researchers involved in designing and analyzing air foils for ...
Pressure-distribution tests have been made in the NACA 4- by 6-foot vertical tunnel of a plain flap with interchangeable beveled trailing edges on an NACA 0009 airfoil. The flap chord was 30 percent of the airfoil chord and the bevel chords were 15 and 20 percent of the flap chord. The...
Experimental investigation of NACA 4415 airfoil using vibration data for stall detectionAirfoil characterizationWind tunnelLow Reynolds numberStall detectionVibrationPurpose\nThe purpose of this study is to identify the possible relation between the vibration and the stall by using the vibration response of...
Experimental/ crystal atomic structure of inorganic compoundsinfrared spectra of inorganic solidslithium compoundsRaman spectra of inorganic substancessodium compounds/ LiMgVO 4LiMnVO 4LiCdVO 4NaCdVO 4NaCaVO 4vibrational spectrumOn the basis of vibrational data and X-ray powder diagrams, the structure ...
A Wind Tunnel Experimental Study of Icing on NACA0012 Aircraft Airfoil with Silicon Compounds Modified Polyurethane Coatings. Materials 2021, 14, 5687. https://doi.org/10.3390/ma14195687 AMA Style Przybyszewski B, Kozera R, Krawczyk ZD, Boczkowska A, Dolatabadi A, Amer A, Sztorch B, ...