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Number of items: 12.

Conference or Workshop Item

Mathur, NB and Yajnik, KS (1989) Axisymmetric afterbody flow separation at transonic speeds in presence of jet exhaust. In: 9th International Symposium on Air Breathing Engines, 03-08 Sept 1989, Athens, Greece.

Proj.Doc/Technical Report

Desikan, KS (1989) Design and commissioning of 0.6M transonic tunnel - mechanical system (project closing report). Project Report. National Aerospace Laboratories, Bangalore.

Dutt, HNV and Jacob, K (1989) Viscous subsonic flow computation for wings with flaps for high-lift. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Krishnamurthy, K (1989) Tests on NAL-114-26-00 symmetric supercritical airfoil in 0.3M Wind tunnel. Project Report. National Aerospace Laboratories, Bangalore.

Krishnan, V (1989) Study of the turbulent boundary layer on an afterbody. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Mohan, KH (1989) Fabrication of 1/20th scale wind tunnel model of jaguar aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Patil, SR and Sridharan, R (1989) Wind tunnel wall corrections to experimental data on wing-body combinations at high angles of attack. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sridharan, R and Ramabhadran, S (1989) A computer code for the estimation of propulsion system installation losses. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Sundaram, S (1989) Calibration of vane anemometer. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Venugopal, S and Krishna Murthy, M (1989) A computer code based on experimental database to estimate the fin alone normal force characteristics upto high angles of attack. Project Report. National Aerospace Laboratories, Bangalore.

Vinay Kumar, - (1989) Experimental studies on a 1/10th scale model of Agni- payload missile. Project Report. National Aerospace Laboratories, Bangalore.

Viswanath, PR and Rajendra, G (1989) Sting-support interference on afterbody drag at transonic speeds. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Wed Apr 23 01:16:31 2014 IST.