Stalling angle predictions of symmetric aero foil by flow analysis

Author:

Santhosh N.,Harish H. V.,Sunil G. S.,Huddar Vivekanand B.,Gowda Ashwin C.,Manjunath N.,Afzal Asif,Razzak Abdul,Praveena B. A.

Publisher

AIP Publishing

Reference24 articles.

1. R Jayakumar, Harish H.V, Santhosh N, Nishant Desai, Srikanth H V, Shrilakshmi V Bentur, Sharmitha, Experimental verification of flow through convergent nozzle using CFD simulation, International Journal of Advanced and Innovative Research, 2278-7844, Volume 3 Issue 9, Pages 34 – 36.

2. Harish H V, Santhosh N, Srikanth H V, Dr M S Raghu, Praveena B A, Amaresha Patil, Shivashankar, Palakshaiah, Optimum Design of Conical Draft Tube by Analysis of Flow Using CFD Simulation, International Journal of Latest Technology in Engineering, Management & Applied Science (IJLTEMAS), Volume 3, Issue 7, July 2014, Pages 99– 103.

3. Harris C. D., “Two-dimensional aerodynamic characteristics of the NACA0012 airfoil in the Langley 8-foot transonic pressure tunnel”. NASA TM-81927; 1981.

4. Transonic unsteady aerodynamic and aeroelastic calculations about airfoils and wings

5. Advances in the computation of transonic separated flows over finite wings

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