Showing 401 - 420 results of 1,473 for search '"Airfoil"', query time: 0.10s Refine Results
  1. 401

    A navier-stokes analysis of airfoils in oscillating transonic cascades for the prediction of aerodynamic damping by Abhari, R, Giles, M

    Published 1997
    “…A numerical study on a generic transonic compressor rotor was performed in which the impact of varying the amplitude of the airfoil oscillation on the normalized predicted magnitude and phase of the unsteady pressure around the airfoil was studied. …”
    Journal article
  2. 402

    Large-eddy simulations of a turbulent Coanda jet on a circulation control airfoil by Nishino, T, Hahn, S, Shariff, K

    Published 2010
    “…Large-eddy simulations are performed of a turbulent Coanda jet separating from a rounded trailing edge of a simplified circulation control airfoil model. The freestream Reynolds number based on the airfoil chord is 0.49 × 106, the jet Reynolds number based on the jet slot height is 4470, and the ratio of the peak jet velocity to the freestream velocity is 3.96. …”
    Journal article
  3. 403

    Numerical study of airfoil stall cells using a very wide computational domain by Manni, L, Nishino, T, Delafin, P

    Published 2016
    “…The formation of stall cells over a NACA 0012 airfoil at a Reynolds number of one million has been investigated numerically, using unsteady Reynolds-averaged Navier–Stokes (URANS) and delayed detached-eddy simulation (DDES) approaches. …”
    Journal article
  4. 404

    Longitudinal aerodynamic characteristics of wau bulan wing-tail configuration with selected airfoil profile by Kusumohadi, Catur Setyawan

    Published 2011
    “…It is a thick airfoil and was designed for low Reynolds number flow. …”
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    Thesis
  5. 405

    Numerical and experimental study of leading edge tubercles with vortex generators on NACA 4415 airfoil by Aftab, Syed Mohammed Aminuddin

    Published 2017
    “…Recently studies have shown that implementing humpback whale Tubercle Leading Edge (TLE), also enhance the performance of the airfoil. The objective of the current work is to combine TLE and VG thereby elimination of separation bubble and increase airfoil lift to drag ratio. …”
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    Thesis
  6. 406

    Lift enhancement of NACA 4415 airfoil using biomimetic shark skin vortex generator by Zulkefli, Nur Faraihan, Ahamat, Mohamad Asmidzam, N. F., Mohd Safri, Mohd Nur, Nurhayati, Mohd Rafie, Azmin Shakrine

    Published 2019
    “…The measurement has been carried out for three considered cases: smooth airfoil for baseline case, airfoil with triangular vortex generator and also airfoil with shark skin shape vortex generator. …”
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    Article
  7. 407

    Analisis Kitaran Melalui Kerajang Airfoil NACA (Lapisan Sempadan) Dan Kawasan Pusaran by Md. Ali, Affandy

    Published 2000
    “…Eksperimen ini adalah berdasarkan kepada tajuk; “Analisis kitaran melalui kerajang airfoil NACA(lapisan sempadan) dan kawasan pusaran”. …”
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    Monograph
  8. 408

    A comparative study of turbulence models on aerodynamics characteristics of a NACA0012 airfoil by Sadikin, Azmahani, Mohd Yunus, Nurul Akma, Abd Hamid, Saiful Anuar, Ismail, Al Emran, Salleh, Salihatun, Ahmad, Sufizar, Abdol Rahman, Mohd Nasrull, Mahzan, Shahruddin, Ayop, Sallehuddin Shah

    Published 2018
    “…This paper presented a computational fluid dynamics (CFD) simulation of air flow past a 2D model NACA0012 airfoil at high Reynolds number (Re = 3.0 x 106 ) at various angles of attack (-10 to 15). …”
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    Article
  9. 409

    Computational fluid dynamic simulation study on NACA 4412 airfoil with various angle of attacks by Abdul Mukhti, Muhammad Ammar Qayyum, Didane, Djamal Hissein, Ogab, Mohammed, Manshoor, Bukhari

    Published 2021
    “…The aerodynamic airfoil blades have a crucial influence on the wind turbine's aerodynamic efficiency. …”
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    Article
  10. 410

    Enhancement on self-starting darrieus bladed wind turbine using J-shape airfoil by Rosmin, Norzanah, Yuni Rahmati, Yuni Rahmati, Evan, Ang Jun Wei, Hatib Musta'Amal @ Jamal, Aede Hatib Musta'Amal @ Jamal

    Published 2022
    “…In this paper, study has been focused to design and develop a modified-Darrieus wind turbine blade based on J-NACA0010, J-NACA0015 and J-NACA0018 airfoil profile. Performance study will be assessed in terms of its self-starting capability, tip speed ratio, angular speed and power output of the proposed system for all the above-mentioned modified airfoils. …”
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    Article
  11. 411

    Aerodynamic noise measurement in anechoic wind tunnel of rod-airfoil with leading edge serrations by Samion, Siti Ruhliah Lizarose, Mat Ali, Mohamed Sukri

    Published 2018
    “…Turbulent flow interaction with the leading edge of an airfoil generates a well-known leading edge noise. …”
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    Article
  12. 412
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  14. 414

    Airfoil selection and computational study on the torque performance of 4-blade vertical axis wind turbine by Sunny, Kalakanda Alfred, Kumar, Pradeep, Kumar, Nallapaneni Manoj, Banerjee, Joy, Adheena, G.J.

    Published 2018
    “…NACA0012, NACA0015, NACA0018 and NACA0021 airfoil types were analysed for the tangential force they create at different angle of attack. …”
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    Conference or Workshop Item
  15. 415

    Robust Algorithm Software for NACA 4-Digit Airfoil Shape Optimization Using the Adjoint Method by Naser Tanabi, Agesinaldo Matos Silva, Marcosiris Amorim Oliveira Pessoa, Marcos Sales Guerra Tsuzuki

    Published 2023-03-01
    “…Optimizing the aerodynamic shape of an airfoil is a critical concern in the aviation industry. …”
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    Article
  16. 416
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  18. 418

    Design of a Mass Air Flow Sensor Employing Additive Manufacturing and Standard Airfoil Geometry by Dimitrios-Nikolaos Pagonis, Vasiliki Benaki, Grigoris Kaltsas, Antonios Pagonis

    Published 2021-12-01
    “…The novelty of the presented sensor focuses on the fabrication process, which is based on additive manufacturing combined with PCB technology, and the design of the sensing elements housing geometry, which is derived through suitable CFD simulations and is based on standard airfoil geometry. The proposed process enables low-cost, fast fabrication, effective thermal isolation, and facile electrical interconnection to the corresponding circuitry of the sensor. …”
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    Article
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