Items where Year is 1970

B

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

C

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.

D

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.

F

Fox, L and Sankar, R (1970) generalised regula falsi. Technical Report. National Aeronautical Laboratory, Bangalore, India.

G

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.

H

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.

K

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.

R

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.

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.

S

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 (1970) Note on the greatest value of the Bijvoet ratio. Acta Crystallographica, A26. pp. 381-382.

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.

V

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.