As you are looking for the Project titles related to Aerodynamics Panel running under DRDO, so here I am sharing the some of them with you

Experimental study of instaneous structure of turbulent flow.
Development of computer programme for evaluation of aerodynamic charateristics of swept wing aircraft.
Development of Mrigasheer Sail Plane.
8" diameter hypersonic wind tunnel.
Hypersonic boundary layer flow of a radiating gas with pressure gradient.
Aeroelastic characteristics of low aspect ratio surfaces.
Cascade study & flow control of airfoils.
Study of jet flows in moving streams.
Structure of shock wave at re-entry speeds ahead of a blunt body.
Design & development of a laser doppler anemometer for measuring velocities in high speed flows.
Design & fabrication of supersonic wing calculator using analogue network.
Analysis of meterological/ aerodynamics data obtained from Canberra aircraft.
Ranganayakamma
Generation of design data in respect of MiG-21 aircraft.
Design and development rarefied gas dynamic facility.
Investigations on atomspheric gusts and their effects on aircraft performance.
Study of turbulent flow over longitudinally curved surfaces.
Augmentation of wind tunnel test facility at NAL, Bangalore.
Analytical and numerical studies of transonic flows around airfoils.
7"x9" intermittent flow down trisonic tunnel
State of art review in transonic aircraft aerodynamics.
Calculation of base drag for aircraft ad missiles configuration.
Flutter analysis of panels in supersonic flow in the presence of boundary layer.
Investigation on transition and drag due to 3-D tripping device.
Development of forced oscillation rig for dynamic stability measurements in high speed wind tunnel.
Design and development of three component balance for use in shock tunnel.
Improvement to open circuit wind tunnel Phase-I.
Study of gas dynamic lasers.
Compilation of computer based hand book for prelimnary design of aircraft.
Study of rotating profile as an aid to control surface design and lift device.
Numerical methods for the design analysis of aerofoils and bodies in subsonic and supersonic flow.
Analysis of transonic flows over airfoils and slendar bodies with viscous longitudinal effects.
Base pressure in subsonic and supersonic flows with particular reference to castellation effects on trailing edges.
A study of flow pattern on around aircraft and missile configuration using coloured liquid technique.
Determination of static and dynamic stability dervatives from flying model tests in shock supersonic tunnel.
Design and fabrication of supersonic wing, calculator using analog network.
Development of a computer programme for evaluation of aerodynamic characteristics of swept wing a/c at transonic.
Design and development of gust tunnel and experimental studies in unsteady aerodynamics.
Theoretical investigation on transonic flow-I.
Study of laminar separation bubble.
Design of supercritical aerofoils and determiantion of their design and off design characteristics.
Shock wave and boundary layer interaction over curved & semi-diamond shaped boundaries with and without injection.
Studies on remotely controlled flight Vehicles (RCFV).
Base flow facility.
Supersonic flow past spiked blunt cones.
Aerodynamic characterisitcs of strake wing.