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Jump to: Proj.Doc/Technical Report Number of items: 17.
Proj.Doc/Technical ReportBalakrishna, S (1970) Wind tunnel pressure regulating systems. Technical Report. National Aeronautical Laboratory, Bangalore, India. Fox, L and Sankar, R (1970) generalised regula falsi. Technical Report. National Aeronautical Laboratory, Bangalore, India. 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. Ramaseshan, S and Viswanathan, KS (1970) Anomalous scattering of neutrons by crystals and the amplitude of vibration of lattice waves. Technical Report. National Aeronautical Laboratory, Bangalore, India. Rangarajan, R and Viswanathan, S (1970) Data reduction program for floating frame balances. Technical Report. National Aeronautical Laboratory, Bangalore,India. Sankar, R and Panchapakesan, S (1970) Solution of a banded system of equations and the calculation of minimum eigen values of large matrices on a small computer. Technical Report. National Aeronautical Laboratory, Bangalore, India. Sankar, R and Panchapakesan, S (1970) Solution of very large systems of equations arising out of biharmonic equations, using iterative methods. Technical Report. National Aeronautical Laboratory, Bangalore, India. 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 Narasimha, R (1970) On the spline approximation for integrals with a logarithmic kernel. 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. Singh, AK and Balasingh, C (1970) Effect of X-ray diffractometer geometrical factors on the centroid shift of a diffraction line for stress measurement. Technical Report. National Aeronautical Laboratory, Bangalore, India. Sridhara, K (1970) Gas making in the dilution zone of a combustions chamber. Technical Report. National Aeronautical Laboratory, Bangalore, India. Srinathkumar, S and Rajanna, D (1970) Differntal transformers. 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, R (1970) An automatic control system for resonance tracking in structural vibration testing. Technical Report. National Aeronautical Laboratory, Bangalore, India. Viswanathan, R and Rao, KS (1970) 240 watt power amplifier. 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. |