Items where Division is "Propulsion Division " and Year is

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Number of items: 17.

J

Jagannatha Rao, B and Chidananda, MS Calibration of fuel bulk meter hal overhaul division 1995. Project Report. National Aerospace Laboratories, Bangalore.

Jagannatha Rao, B and Chidananda, MS and Krishna Kumar, VS Calibration of pitot – static probes for H.A.L., Koraput. Project Report. National Aerospace Laboratories, Bangalore.

K

Khan, AA and Vyas, VK and Muthu Selvan, G and Satish Kumar, M and Hariharan, R and Muralidhara, HS Design and erection of exhaust system for small gas turbine engine test facility. Project Report. National Aerospace Laboratories, Bangalore.

L

Lingarkar, E and Sankaranarayanan, S Cryogenic Turbopump Testing at NAL. Project Report. National Aerospace Laboratories, Bangalore.

M

Murugesan, K and Ramamurthy, S Component Drawings for Compact By-Pass Engine. Project Report. NAL, NAL Bangalore. (Submitted)

Murugesan, K and Ramamurthy, S Determination of Pressure Distribution on Blade Cascades. Project Report. NAL, NAL Bangalore. (Submitted)

Murugesan, K and Ramamurthy, S and Sankaranarayanan, S Feasibility study of small gas turbine engine development. Project Report. NAL, NAL Bangalore. (Submitted)

N

Naik, NK and Veera Sesha Kumar, C Ballistic impact behavior of foam core sandwich structures: Formulation. In: International Conference on Composites - Current and Future Trends, Indian Institute of Science.

R

Rajashekar, C and Bhaskaran, M and Srinivas, J and Prateesh Kumar, P and William Grips, VK and Aruna, ST and Venkat Iyengar, S Experimental studies on a liquid fuelled medium scaled valved pulsejet. In: 22 nd National Conference on IC Engines and Combustion, 10 - 13 December 2011, NIT Calicut.

Ramamurthy, S and Arunkumar, V and Prabhu, BS Application of Aerodynamic foil bearing in high speed spindles of textile machinery –case study. In: International Conference on Tribology AUSTRIB 1994, Australia.

Ramamurthy, S and Sankaranarayanan, S and Murugesan, K and Ramachar, D and Rajendran, R Development of High Pressure ratio Centrifugal Compressor Stage. In: 4th National Conference on Air Breathing Engines and Aerospace Propulsion, 1998 December, Bangalore. (Submitted)

S

Sankaranarayanan, S and Ramamurthy, S and Murugesan, K and Ramachar, D and Rajendran, R Flow Investigation in Centrifugal Compressor Diffuser. In: Workshop on Experimental Fluid Mechanics and Turbomachinery. (Submitted)

Sankaranarayanan, S and Roshan, Antony and Suraj, CS Technology Driven Programme for the Development for the Development of a Fixed wing micro Air Vehicle at NALDRIVEN. In: MAV Workshop- Challenges and Presferred Outcomes, 13 November 2008, National Aerospace Laboratories.

Senthil Kumaran, R and Swamy, KMM and Suraj, CS Experimental investigations on semi-cryo rocket engine turbo pump turbine profiles part-I nozzle profile. Technical Report. National Aerospace Laboratories, Bangalore.

Shobhavathy, MT and Prathapanayaka, R and Jayaraman, M and Dileepkumar B , Alone and Satishkumar, S and Samiullah, TH and Rajagopal, RS and Janaki Rami Reddy, M Development of a High Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blads. Project Report. NAL, Bangalore.

T

Thennavarajan, S and Ramamurthy, S and Janaki Rami Reddy, M and Pandian, K PRESSURE DROP TEST ON LCA FUEL SYSTEM LRU’s. Project Report. NAL, NAL.

V

Venkatesh, S and Jagannatha Rao, B and Chidananda, MS Calibration of Fuel Rotameters (HAL NASIK) Division 1991. Project Report. National Aerospace Laboratories, Bangalore.

This list was generated on Thu Jun 1 17:40:57 2023 IST.