Items where Author is "Altaf, Afaq"

Article

Mohammed Aldheeb, Mohammed Abdulmalek and Asrar, Waqar and Omar, Ashraf Ali and Altaf, Afaq and Sulaeman, Erwin (2020) Effect of a directionally porous wing tip on tip vortex. Journal of Applied Fluid Mechanics, 13 (2). pp. 651-665. ISSN 1735-3572 E-ISSN 1735-3645

Mohammed Aldheeb, Mohammed Abdulmalek and Asrar, Waqar and Omar, Ashraf Ali and Altaf, Afaq and Sulaeman, Erwin (2020) Aerodynamics of symmetric permeable airfoils and wings: CFD simulation. Progress in Computational Fluid Dynamics, 20 (6). pp. 349-361. ISSN 1468-4349 E-ISSN 1741-5233

Altaf, Afaq and Tan, Boon Thong and Omar, Ashraf Ali and Asrar, Waqar (2016) Impact of a reverse delta type add-on device on the flap-tip vortex of a wing. International Journal of Aviation, Aeronautics, and Aerospace, 3 (3). pp. 1-28. E-ISSN 2374-6793

Altaf, Afaq and Omar, Ashraf Ali E. and Asrar, Waqar (2011) Study of the reverse delta wing. Journal of Aircraft, 48 (1). pp. 277-286. ISSN 0021-8669

Proceeding Paper

Altaf, Afaq and Thong, Tan Boon and Omar, Ashraf Ali and Asrar, Waqar (2017) Experimental investigation of the influence of a reverse delta type add-on device on the flap-tip vortex of a wing. In: 3rd International Conference on Mechanical, Automotive and Aerospace Engineering 2016 (ICMAAE’16), 25th-27th July 2016, Kuala Lumpur, Malaysia.

Asrar, Waqar and Altaf, Afaq and Omar, Ashraf Ali and Hrairi, Meftah and Thong , Boon Tan (2015) Aerodynamic performance of a naca 23012 half wing model with a reverse delta wing type add-on device. In: 8th Ankara International Aerospace Conference, 10-12 Sep 2015, Ankara, Turkey.

Altaf, Afaq and Omar, Ashraf Ali E. and Asrar, Waqar and Ludin@Jamaluddin, Hani (2011) Investigation of the vortical flow around a reverse delta wing. In: International Conference on Mechanical, Automotive and Aerospace Engineering 2011 (ICMAAE11) , 17-19 May 2011, Legend Hotel, Kuala Lumpur .

Altaf, Afaq and Omar, Ashraf Ali E. and Asrar, Waqar (2010) Experimental investigation of the vortical flow around a reverse delta wing using PIV. In: Experimental Fluid Mechanics 2010, 24-26 November 2010, Liberec / Czech Republic.