Configuration design for PDE combustor
| PI Details | Co-PI Details |
|---|---|
|
Dr T K Jindal
Designation: Professor |
| Funding Agency | Project Cost |
|---|---|
| TBRL Chandigarh |
Rs. 9.38 |
| Start Date | Completion Date | Status |
|---|---|---|
| 2016-07-27 | 2019-03-31 | Completed |
Abstract
The project form TRRL was undertaken the development of PDE combustor with flow control system, fire control system and data acquisition from the no of tests. The development was undertaken successfully and the firing proved to be consistent every time. The data w.r.t pressure and thrust was captured for the tests and the performance curves were obtained.
| Manpower Sanctioned/Hired | Manpower Trained |
|---|---|
|
Ph.D Produced: 2 |
Equipment Sanctioned/Procured
|
Name of Equipment |
Make & Model |
Year of Purchase |
Cost |
Salient Features of Equipment |
Condition (Working /Not Working) |
|---|---|---|---|---|---|
|
Flow control system |
|
|
5.00 Lakh |
Flow control system for Acetylene and oxygen flow control |
Working |
Publications
List of SCI Publications under Project
|
Authors Name |
Title of Paper |
Journal Name |
Volume |
No. |
Page No. |
Year |
DOI Number |
|
B A Dogra |
A Characterized Status Report on Pulse Detonation Engine |
INCAS Bulletin |
11 |
2 |
69-83 |
2019 |
10.13111/2066-8201.2019.11.2.6 |
|
B A Dogra |
Technological advancements in Pulse Detonation Engine Technology in the recent past: A Characterized Report |
INCAS Bulletin |
11 |
4 |
81-92 |
2019 |
10.13111/2066-8201.2019.11.4.8 |
|
B A Dogra |
Analysis of Equivalence Ratio in an Oxygen Acetylene Mixture
|
INCAS Bulletin |
11 |
4 |
171-177 |
2019 |
10.13111/2066-8201.2019.11.4.15 |
|
S Dhama |
Thrust Augmentation of Single Cycle Pulse Detonation Engine using Nozzles |
Int. J. Vehicle Structures & Systems |
13 |
1 |
80-85 |
2021 |
10.4273/ijvss.13.1.16 |
|
S Dhama |
Influence of Nozzle Type, Divergence Angle and Area Ratio on Impulse of Pulse Detonation Engine |
INCAS Bulletin |
12 |
2 |
35-45 |
2020 |
10.13111/2066-8201.2020.12.2.4 |
|
T K Jindal |
Proposed thrust profile design of Pulse Detonation Engine for Aerospace Applications |
Springer, Advances in Energy and Combustion, 2021 |
-- |
-- |
85-102 |
2021 |
10.1007/978-981-16-2648-7_4 |
|
Udit Vohra, Rajpreet Singh, Vinayak Bassi, T. K. Jindal, and Amarjit Singh |
Numerical Study of Deflagration to Detonation Transition in 2D and Axisymmetric Detonation Tube with Obstacles Using OpenFOAM
|
Advances in IC Engines and Combustion Technology |
-- |
-- |
807-820 |
2021 |
10.1007/978-981-15-5996-9_62 |
Output/Outcome of the Project
Output/Outcome of the project
The test rig has been developed with successful design of fire control system and flow control system. The data acquisition system was commissioned as per the requirement. The control system was developed on two options viz. through Lab view and through mobile from a distance.