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Number of items: 25.

Desikan, KS (1974) Design of a force balance calibration rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Desikan, KS (1974) Design of acoustic mufflers for blowdown wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Dwarakanath, GS and Ramamoorthy, P and Rao, DM (1974) Evaluation of the transonic wave drag integral with particular reference to a real aircraft. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Gopinath, R and Murthy, AV (1974) Numerical solutions of the compressible, laminar boundary layers with pressure gradients at large pfandtl numbers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gupta, Ramesh P (1974) New design of pressure probe as a skin friction gauge. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Gupta, Ramesh P (1974) A technique for flow measurement in separated flow. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nagpurwala, QH and Mohan, K (1974) Proposed instrumentation for compressor research rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Paranjpe, PA and Murugesan, K (1974) Role of machinery centre for power sector. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Pattanaik, S and Gopinathan, KG and Arunachalam, VS (1974) Dispersion hardened titanium alloys by powder metallurgy. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Pureswaran, Shankar and Santhanam, A (1974) Instrumentation for fluidic temperature sensor. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramaswamy, MA (1974) Application of integral moment method to the hypersonic laminar near wake of a cold cylinder. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Ramaswamy, MA and Sharma, Ramachandra and Krishnamuthy, K (1974) Two dimentional transonic blockage interference studies in the NAL 1-Ft. blowdown wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Seshadri, SN and Rajendra, G (1974) Appplication of the method of axial source for calculation of subcritical pressure distribution on 'Not'slender axisymmetric bodies at zero lift. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Seshadri, SN and Rao, DM (1974) On the application of radial-splitters flow spreaders in the NAL 1-FT. blowdown tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Singh, Karan and Murugesan, K (1974) Design of a highly loaded gas turbine stage. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Ramaswamy, MA (1974) Preliminary results of the computation of pressure distribution on a super critical aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sinha, UN and Ramaswamy, MA (1974) Priliminary results of the computation of pressure distribution on a supercritical aerofoil. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sivasankaram, K and Sridhara, K (1974) Some experimental studies on aerodynamic and bluffbody flameholders. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sridhara, K and Thunga, KS (1974) Design and development of a cold air turbine. Technical Report. National Aerospace Laboratories, Bangalore,India.

Subrahmanyam, S and Murthy, GK and Paranjpe, PA (1974) Pyrogenic ignition system for afterburners. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Suryanarayana, BG (1974) Design of a sidewall mounted model injection system for the NAL 1x2019; x 1x2019; trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Suryanarayana, BG (1974) Design of a sidewall-mounted model incidence system for the N.A.L. l' X l' Trisonic Wind Tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Suryanarayana, BG (1974) Some design considerations for a transient load protection system for aeroelastic testing of rocket models in the NAL blowdown tunnel. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Varute, PT and Samraj, AC (1974) Development of pressure regulating valve for cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Viswanathan, R and Baghialakshmi, S (1974) Voltage controlled two phase func generator using op-amps. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Tue Oct 21 01:06:07 2014 IST.