dc.contributor.author |
Singh, Ritesh |
|
dc.date.accessioned |
2025-02-04T12:03:57Z |
|
dc.date.available |
2025-02-04T12:03:57Z |
|
dc.date.issued |
2024-03 |
|
dc.identifier.citation |
Under the guidance of Dr. Om Prakash, Professor, UPES ; Dr. Sudhir Joshi, Professor, Graphic Era University & Dr. Yogananda Jeppu, Honeywell Technology Solutions, Hyderabad |
en_US |
dc.identifier.uri |
https://dr.ddn.upes.ac.in//xmlui/handle/123456789/4400 |
|
dc.description |
Thesis submitted in partial fulfillment of the requirements for the award of the Degree of Doctor of Philosophy (Aerospace Engineering) |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
School of Advanced Engineering, UPES, Dehradun |
en_US |
dc.subject |
Thesis |
en_US |
dc.subject |
Aerospace Engineering |
en_US |
dc.subject |
Airbreathing Hypersonic Model |
en_US |
dc.subject |
Flight Dynamic Simulation |
en_US |
dc.subject |
Trim Analysis |
en_US |
dc.subject |
Bifurcation Analysis |
en_US |
dc.subject |
Close Loop Simulation |
en_US |
dc.title |
Flight dynamics analysis of generic airbreathing hypersonic vehicle using bifurcation method |
en_US |
dc.type |
Thesis |
en_US |