Industrial Projects

Dronesapp is a service booking marketplace platform for Drone Industry. Here are we are developing a platfrom to fill the gap between service providers and users of Drones. we are also trying to make this platform as one stop solution for all drone needs.


Utilizing cloud-based technology, we employed Insights to gather data and meticulously analyzed both lidar and image data, leaving no feature unnoticed. Our dedicated team of 38 employees collaborated to process this data, ensuring that it adhered to the highest quality standards for Cyient for a period of 4months. As a result of our efforts, we successfully generated digital replicas of the road networks and electrical infrastructure, faithfully mirroring the provided dataset. 


Over a span of 1.6 years, a dedicated team of 22 employees undertook the task of digitizing a vast array of features, encompassing more than 2000+ square kilometers of mapping. Working in two shifts as per the requirements of our esteemed client, Coderize, our employees diligently produced the following dataset:

Leveraging Google Maps data, we meticulously determined the exact dimensions, including height and area, of various elements such as buildings, vegetation, canals, rivers, and more. This extensive dataset was crafted at the specific request of our client, covering over 1200 square kilometers of data in Japan, USA, and Europe. 

Acadamic Projects

The study is to design a 2-D supersonic nozzle with pores at various locations for thrust vectoring. Need to study the shock angle, due to injection of fluid at the various location from throat to the edge of the nozzle and various injection angles (30, 45, 60, 90)degrees. Finally need to conclude with vectoring angle and limits of vectoring


A deep understanding and designing of a Scaled Ramjet Engine with different operating conditions which range from Mach -2.5 to 4.5 with an increase of 0.5Mach increase. Maximum fuel consumption and shock distribution are studied to understand the operating of the ramjet engine. The study is performed for both cold flow and combusted flow. Hence we concluded as for the low Mach speed fuel consumption is too high whereas for higher Mach speeds fuel consumptions are low. We also came to an understanding of limitations initial and final speed as the engine couldn't operate for speed of Mach<2 and it couldn't operate for Mach>4 it is concluded by studying chocking conditions.

When a blunt geometry vehicle traveling hypersonic speeds undergo high thermal load. During such speed, they travel through various flow regimes with different density in the atmosphere due they encounter high temperatures and heat flux on the wall. In this paper, we discuss new methods for reducing drag and temperature at such speeds. In such cases, we ended up by changing the Knudsen number decreasing density and pressure of the atmosphere. During our study, we found that body undergoes high pressure and observed increasing Kn number reduced drag.

A study is performed to understand Deflagration to Detonation process. Computational Fluid study gave us a proper understanding of the DDT process and the process of conducting the Detonation wave. This study concluded with maximum pressure wave generated in the DDT tube and time taken for single pulse generation, Fuel consumption and Combustion process. Further studies need to be performed for the continuous pulse generation process.

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This work is based on study of Nose cone design for hypersonic missiles. The 2-D Profile is used to study shock wave, Shock standoff distance, Thermal properties, and drag observed due to an increase in nose bluntness. Nose cone starting from sharp edge to blunt nose by varying nose radius with a variation of 0.5D is studied and finally concluded with drag and thermal study.

This study gave us an understanding in reducing the thermal loads on the blunt nose cone bodies which travel in supersonic speeds. In the continuation to study of nose cones, addition of spikes yielded best results comparitively. Hence using of spikes( Blunt Nose, Arrow Spike, Aerodisk, Hemespherical Spike) are studied and finally concluded that Hemespherical Spike yields best results comparatively. This gave us a proper understanding on the design parameters of selection of limits to spike shape and its length.

Design and optimization of pressure vessels (Spherical, Cylindrical, Obround, and Ellipse) to sustain a pressure of 60bar using Ansys FEM analysis. The study finally concluded by saying Spherical vessel yielded less mass for both AA6060-T651 and Ti6Al4V. This also stated that Titanium materials have less mass comparing with AA materials. We also concluded the Heat affect zone limits to what extent it needs to be maintained.

The study on the effects of fiber orientations on a four-layer composite plate under pressure load using the FEM tool are performed using Ansys Mechanical APDL. The orientation studied are i) 0, +90, -90, 0. ii) 0, +45, -45, 0. iii) 0, +45, -45, 0. Results conclude structural behavior and load-carrying capacity of the material.