Design Aircraft
Resume:
CHERUKURI JAGANNADHA RAO
**************@*****.***
D.No: 1-1-57/16, Vavilal Nagar, Atchampet Road, Sattenapalli, Guntur Dist, Andhra Pradesh, 522403.
https://www.linkedin.com/in/jagannadha-rao-cherukuri-198280167 Objective
To work in a firm with a professional work driven environment where I can utilize and apply my knowledge, skills which would enable me as a fresh graduate to grow while fulfilling organizational goals. Education
Veltech Rangarajan Dr. Sagunthala R&D Institute of Science and Technology B.Tech/ Aeronautical engineering
7.74
Narayana Junior College
Intermediate
930
Holy Family English Medium High School
S.S.C
9.5
Skills
CATIA
Ansys Workbench
MS Office
MS Excel
Hypermesh
Projects
Optimum design of a small wind turbine blade for maximum power production The rotor blades of a wind turbine are critical components that consist of aerodynamic shapes called airfoils. The interaction of these airfoils with the wind allows converting the power in the wind to mechanical power. The structure of the rotor blades must be able to extract maximum energy from the wind while being strong enough to stand steady, periodic and randomly changing loads. For maximum power extraction, an optimum design of the rotor blades is necessary. This is a typical design methodology of the rotor blades of a small wind turbine with a power generation of 3.5 KW to 5 KW (rotor radius of 2.4m). First, the design parameters were presented. Then, optimum blade geometry (chord length and twist angle distribution) was determined. Finally, the wind turbine blade performance was assessed.
Design of a Cargo aircraft
There are several factors that need to be taken into account while designing an aircraft. Most aircraft are passenger- oriented, others are designed for cargo and others combine the both. Regardless of the aircraft purpose, issues such as fuel-efficiency, engine performance, maintenance costs and route requirements are necessary elements of aircraft design. Aircrafts that are cargo-oriented or take into account cargo requirements on passenger routes must also considered cargo capacity in their design. The aim of this report, is to present an application of the design procedure followed in the course entitled “Aircraft Design”. A cargo aircraft at 6944.14km about an endurance of 8.3 hrs at a cruise speed of 822.3kmph. The project involves the design of a medium cargo aircraft that carry payload about 40000 kg.
Increasing launching capability of a fixed wing aircraft In this project, a concept of a UAV (unmanned aerial vehicle) bungee catapult is analyzed by introducing an appropriate combination of elastic and non-elastic cords which significantly increases efficiency (by decreasing of power losses) compared to a widely spread concept of bungee catapult with elastic cords only. This enables installing a few times greater number of elastic bungee cords into the same modular space in the bungee catapult. The concept of elastic and non-elastic cords gives the bungee catapult a possibility to hand over to a UAV more than twice greater launch energy in relation to the concept of elastic cords only. Also, in this project, a mathematical model of UAV new bungee catapult with elastic and non-elastic cords is given, as well as the analysis comparing the new energy loses of both concepts.
Design of a business jet
The main aim of the project is to design the prototype of the business jet of passengers ranges from 15 to 20 having high speed and high range aircraft that can cover the distance with less endurance.
Language
English
Hindi
Telugu
Tamil
Kannada
Personal Details
Date of Birth : 22/01/1999
Nationality : Indian
Internships
CAD Design
Wish Energy Solutions Pvt. Ltd, Wagholi
Sep 2019 - Apr 2020
Optimum design of the rotor blades. This is a typical design methodology of the rotor blades of a small wind turbine with a power generation of 3.5 KW to 5 KW
(rotor radius of 2.38m).
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