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Number of items: 8.

Balakrishna, S (1970) Wind tunnel pressure regulating systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Desai, SS and Jain, RK (1970) A method of curvature matching for two dimensional flexible plate wind-tunnel nozzles. AIAA Journal, 8 (11). pp. 2105-2106.

Gopinath, R and Subramanian, NR (1970) Study of the asymptotic behaviour of compressible laminar boundary layers of a dissociating gas. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rao, DM (1970) Hypersonic aerodynamic characteristics of flat delta and caret wing models at high incidence angles. Journal of Spacecraft and Rockets, 7 (12). pp. 1475-1476.

Seetharam, HC and Rangarajan, R (1970) Force calibration of AGARD B model in transonic flow mach numbers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Shanbhag, VV and Rao, RU (1970) Formal force characteristics of cone-cylinder and ogive cylinder bodies at mach number = 1.8. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Varute, PT (1970) Setting up hydraulic/pneumatic systems facility at National Aeronautical Laboratory. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Viswanathan, S (1970) Programs to analyze supersonic flow past right circular cones with a view to make use of uncalibrated cones for determination of flow angles and mach numbers in wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Sat Apr 19 01:16:00 2014 IST.