Items where Author is "Murthy, MVA"

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Number of items: 12.

Proj.Doc/Technical Report

Murthy, MVA and Muralikrishna, Radha V (1998) TURBOPLOT-Post processor graphics software for CFD analysis of turbomachines. Technical Report. National Aerospace Laboratories, Bangalore, India.

Chandrappa, BK and Krishnamurthy, SJ and Krishnamoorthy, V and Murthy, MVA and Murugesan, K and Pai, BR and Ramachandra, MS and Ramamurthy, S and Swamy, KMM and Shembharkar, TR and Soundranayagam, S (1992) Aerodynamic and Heat Transfer Studies of HPT Rotor and Stator Blades of GTX-35-VS Engine. Project Report. NAL, NAL Bangalore.

Chandrappa, BK and Krishnamurthy, SJ and Krishnamoorthy, V and Murthy, MVA and Murugesan, K and Pai, BR and Ramachandra, MS and Ramamurthy, S and Swamy, KMM and Shambarkar, TR and Soundranayagam, S (1991) Aerodynamic and Heat Transfer Studies on HUB sections of a high pressure turbine blade: summary report. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, MVA and Subramanian, PS (1991) Instrumentation for kaveri HP turbine stage test. Project Report. National Aerospace Laboratories, Bangalore.

Krishnamurthy, SJ and Murthy, MVA (1991) Theoretical predictions of flow distribution in cascades of HP turbine blade HUB section. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, MVA and Thunga, KS (1990) Design review on the project turbo power pack Phase I. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, SJK and Murthy, MVA and Shembharkar, TR (1989) Theoretical Evaluation of H.P Turbine Blade profiel sections for GTX-35 VS Engine. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, MVA and Thunga, KS and Murthy, SJK (1989) Turbo power pack - Phase I. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, MVA and Srinivasa, C (1986) Relative Flow Mach Number Distribution on the Blade PD PR 8606 Profiles of a Turbine Stage. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, MVA and Srinivasa, C (1985) Mach number distribution on blade to blade surface of a turbine stator pasage. Project Report. National Aerospace Laboratories, Bangalore.

Murthy, MVA and Paranjpe, PA (1977) Test facility for performance evaluation of model turbine stages. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Murthy, MVA and Paranjpe, PA (1977) Turbine test facility of Propulsion Division. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Fri Oct 31 04:05:14 2014 IST.