Proposed Thrust Profile Design of Pulse Detonation Engine (PDE) for Aerospace Applications
S Chander, TK Jindal - Advances in Energy and Combustion: Safety and …, 2022 - Springer
The paper deals with challenging assignment of development and optimization of pulse
detonation engine (PDE) to test it in aerospace system configurations. Our researchers have …
detonation engine (PDE) to test it in aerospace system configurations. Our researchers have …
Application of Anova to pulse detonation engine ground demonstrator's dynamic performance measurements
S Chander, R Kumar, M Sandhu… - 2017 First International …, 2017 - ieeexplore.ieee.org
Application of Anova to Pulse Detonation Engine ground demonstrator's dynamic
performance measurement is being explored due its large data of chamber pressure at …
performance measurement is being explored due its large data of chamber pressure at …
[PDF][PDF] New Electrical Design for Pulse Detonation Test Rig
S Chander, TK Jindal - … in Advancements and Futuristic Trends in …, 2015 - researchgate.net
The design of a cyclic Pulse Tube for detonation of gaseous fuel using C2H2 & O2 was
derived from single shot Pulse Detonation Engine (PDE) system in 2014. During the trials of …
derived from single shot Pulse Detonation Engine (PDE) system in 2014. During the trials of …
[PDF][PDF] Design of Sensor Data based Control on Pulse Detonation Engine for Aerospace
TK Jindal - csjournals.com
Application of various types of sensors to Pulse detonation engine to predict the dynamic
performance and its control, which has resulted in quantifying engine functionality during …
performance and its control, which has resulted in quantifying engine functionality during …
PERFORMANCE ENHANCEMENT OF AEROSPACE VEHICLE OF PULSE DETONATION ENGINE (PDE)--PHASE-II
S Chander, TK Jindal - Indian Journal of Scientific Research, 2017 - go.gale.com
PDE is emerging aerospace propulsion system option due its simpler construction, high
impulse, small form factor and light weight up to hypersonic velocities. A large numbers of …
impulse, small form factor and light weight up to hypersonic velocities. A large numbers of …