Now showing items 1-5 of 5

    • Aerodynamics Analysis of F-16 Aircraft 

      Peiris, HAM; Nirmal, PVS; Bandara, HMHHS; Mahindarathne, DM; Rangajeeva, SLMD; Bandara, RMPS (2015)
      The Lockheed Martin F-16 Fighting Falcon is the world’s most prolific fighter with more than 2000 in service. The primary objective of this research project is to evaluate the aerodynamics behaviour of the F-16 aircraft ...
    • Airborne Measurement – Advanced Instrument Development Methods and Insight 

      Lawson, NJ (2018)
      Airborne measurement is required in many fields of aerospace, ranging from aircraft development and flight test, to atmospheric sciences. It involves the use of aircraft mounted instruments to measure quantities ranging ...
    • Assessment of aerodynamic behaviour of the NACA 64A212 airfoil on the context of computational fluid dynamics 

      Bandara, RMPS; Abeygoonewardena, JI (2013)
      A comprehensive understanding of an aircraft�s fluid and flight dynamics cannot be understated from both an engineering and aircraft handling perspective. In this context, availability of such descriptive information, ...
    • Development of a Budget Roof Fairing Using a CFD Analysis of Different Roof Fairing Shapes 

      Wickramasinghe, HD; Jayawardana, WAIS; Wijerathne, THDD; Rangajeeva, SLMD (2018)
      Semi-trailer trucks are commonly used in Sri Lanka for long distance transportation. These trucks are subjected to an unfavourable high drag which makes a huge impact in fuel consumption. In order to reduce this drag, ...
    • Helicopter Main Rotor aerodynamic simulation with CFD 

      Perera, GAPR; Jagathsinghe, HDH; Dilshan, SKK; Sudaraka, MAM; Rangajeeva, SLMD (2016)
      The Bell 212 helicopter is one of the major general purposes utility rotorcraft currently in use in SLAF which is containing NACA 0012 aerofoil in the two blades of main rotor. The primary objective of this research project ...