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Chandra, Ramesh and Basava Raju, B (1970) Stresses around a circular hole in a shallow conical shell with torsional loading. International Journal of Solids and Structures, 6 (10). pp. 1389-1401.
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.
Hebbar, Sheshagiri K and Sridhara, K and Paranjpe, PA (1970) Performance of conical jet nozzles in terms of discharge coefficient. Journal of Aeronautical Society of India, 22 (1). pp. 3-9.
Hussainy, SA and Hasseem, Mohamed H and Bhagawan, GK (1970) Stress distribution in the vicinity of slender notches having arbitrary shapes. Experimental Mechanics, 10 (1). pp. 46-48.
Kariappa, - and Somashekar, BR and Shah, CG (1970) Discrete element approach to flutter of skew panels with13; in-plane forces under yawed supersonic flow. AIAA Journal, 8 (11). pp. 2017-2022.
Kariappa, V and Somashekar, BR (1970) Flutter of skew panels by the matrix displacement approach. The Aeronautical Journal of the Royal Aeronautical Society, 74 (716). pp. 672-675.
Krishnan, A and Krishnan, S (1970) Effect of a diode across the spark gap in electric discharge machining. Indian Journal of Technology, 8 (10). pp. 388-390.
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.
Singh, AK (1970) Note on the greatest value of the Bijvoet ratio. Acta Crystallographica, A26. pp. 381-382.
Balakrishna, 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.
