Items where Subject is "Mechanics of flight: Aerodynamics"

Group by: Creators | Item Type
Number of items at this level: 23.

Article

The effect of injection pressure on the droplet size distributions and micro-explosion / Mhadi A. Ismael ... [et al.]. (2018) Journal of Mechanical Engineering (JMechE), SI 7 (1). pp. 91-102. ISSN 18235514

The Effect of Elevons Deflection to Aerodynamic Coefficients of A Tail-less Blended Wing-Body Planform / Rizal E. M. Nasir ...[et al.]. (2017) Journal of Mechanical Engineering (JMechE), SI 4 (4). pp. 151-166. ISSN 18235514

Large-eddy simulation of unsteady pitching aerofoil using a oneequation subgrid scale (SGS) model based on dynamic procedure / Firdaus Mohamad and Takeo Kajishima. (2021) Journal of Mechanical Engineering (JMechE), 8 (1). pp. 157-173. ISSN (eISSN):2550-164X

Aerodynamics Performance of Barn Swallow Bird at Top Speed : A Simulation Study / M.R.M. Nawi and M.S.A. Azhar. (2018) Journal of Mechanical Engineering (JMechE), SI 5 (5). pp. 1-15. ISSN Journal of Mechanical Engineering (JMechE)

Unravelling tool edge trajectory patterns: Implications on surface roughness in end milling process / Fatiha Naziera Yusof, Mohd Fauzi Ismail and Rizal Mohamed Noor. (2023) Journal of Mechanical Engineering (JMechE), 12 (1): 5. pp. 81-99. ISSN 1823-5514 ; 2550-164X

Experimental Investigation of Effects of Wing Camber on Drag for a Bio-Mimic MAV Flapping Wing / H. Yusoff ... [et al.]. (2018) Journal of Mechanical Engineering (JMechE), SI 5 (5). pp. 16-28. ISSN 18235514

Thesis

Aerodynamic study on go-kart using computer aided tools / Mohd Yusri Abu Bakar. (2005) Degree thesis, thesis, Universiti Teknologi MARA (UiTM).

To study and simulate the concept of ramjet / Amiruddin Amkaromi. (2005) Degree thesis, thesis, Universiti Teknologi MARA.

Behaviour of symmetrical and asymmetrical geometries in fully immersed flow / Fauziah Jerai @ Junaidi. (2007) Masters thesis, thesis, Universiti Teknologi MARA.

Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali. (2015) PhD thesis, thesis, Universiti Teknologi MARA.

Study of short period behaviour for BWB UAV / Mohd Safuan Rosli. (2009) Degree thesis, thesis, Universiti Teknologi MARA Shah Alam.

3D experimental of air flow analysis around Proton Savvy car model / Mohd Anuar Affendi Senardi. (2006) Degree thesis, thesis, Universiti Teknologi MARA (UiTM).

Student Project

Aerodynamic performance of MAV wing with fuselage and stabilizer \ Muhammad Izzuddin Arif Abdul Samad. (2017) [Student Project] (Unpublished)

Induced drag analysis of multi-winglets for aerodynamic performance on NACA 23015 / Zaim Ariefin Azwan Affendi Nual. (2020) [Student Project] (Unpublished)

Aerodynamics performance of optimal wing profile on MAV wing / Siti Khatijah Hamdan. (2017) [Student Project] (Unpublished)

Aerodynamics performance of optimal wing profile on MAV wings / Siti Khatijah Hamdan. [Student Project] (Submitted)

Aerodynamic performance of O-ring paper plane \ Amirul Ashraf Hassan. (2017) [Student Project] (Unpublished)

Experimental aerodynamics of washout twist morphing MAV wing / Muhammad Hakim Mohd Hafiz. (2017) [Student Project] (Unpublished)

Design, manufacture and testing an aircraft model / Mohd Izzed Mustaffa ... [et al.]. (2001) [Student Project] (Unpublished)

An aerodynamic performance of MAV wings / Nik Muhammad Muzammil Nik Mustapa. (2016) [Student Project] (Unpublished)

Research Reports

Interception loss canopy cover, C formulation theory / Azinoor Azida Abu Bakar … [et al.]. (2013) [Research Reports] (Unpublished)

Experimental determination of the effect of turbulent intensity on aerodynamic characteristics of Remotely Piloted Vehicle / Zurriati Mohd Ali, Ow Chee Sheng and Mohd Zulkifly Abdullah. (2007) [Research Reports] (Unpublished)

Aerodynamics prediction of multi-purpose UAV using wind tunnel experimental approach / Ghazirah Mustapha @ Mustafa, Zurriati Mohd Ali, Wirachman Wisnoe. (2009) [Research Reports] (Unpublished)

This list was generated on Fri Apr 26 07:05:28 2024 UTC.