Aerodynamic Characteristics of the Wing Airfoil NACA 43018 in Take Off Conditions with Slat Clearance and Flap Deflection-Reference-Cited by-同舟云学术

Aerodynamic Characteristics of the Wing Airfoil NACA 43018 in Take Off Conditions with Slat Clearance and Flap Deflection

Published:2022-08-19 Issue: Volume: Page:220-229
ISSN:2195-4356
Container-title:Lecture Notes in Mechanical Engineering
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Author:

Hariyadi S. P. Setyo^ORCID,Pambudiyatno Nyaris,Sutardi ^ORCID,Fungky Dyan P.

Publisher

Springer Nature Singapore

Link

https://link.springer.com/content/pdf/10.1007/978-981-19-0867-5_27

Reference11 articles.

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2. Traub LW, Kaula MP (2016) Effect of leading-edge slats at low Reynolds numbers. Aerospace 3. https://doi.org/10.3390/aerospace3040039

3. Yahyaoui M (2014) Generalized vortex lattice method for predicting characteristics of wings with flap and Aileron deflection. 8:1660–1668

4. Askar M, Eng Mohammed Kheiraldeen Abbas A, Hasan Khudhur Abbas E (2016) Aerodynamic study of Slot Effect on ClarkY-14 in low speed wind tunnel engineering analysis with ANSYS software view project aerodynamic study of slot effect on ClarkY-14 in low speed wind tunnel. Int J Art Human Sci (IJAHS) www.ijahs.com 3:21–29

5. Mulvany N, Chen L, Tu J, Anderson B (2004) Steady-state evaluation of two-equation RANS (Reynolds-Averaged Navier-Stokes) turbulence models for high-reynolds number hydrodynamic flow simulations. Department of Defence, Australian Government, pp 1–54

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1. Aerodynamic And Aeroacoustic Study Of Using Multiple-Element-Wing Leading-Edge Slat On Plain And Slotted Flap Wing Airfoil NACA 43018;J APPL SCI ENG;2024