Flight dynamics analysis of generic airbreathing hypersonic vehicle using bifurcation method

Simple item page
dc.contributor.authorSingh, Ritesh
dc.date.accessioned2025-02-04T12:03:57Z
dc.date.available2025-02-04T12:03:57Z
dc.date.issued2024-03
dc.descriptionThesis submitted in partial fulfillment of the requirements for the award of the Degree of Doctor of Philosophy (Aerospace Engineering)en_US
dc.identifier.citationUnder the guidance of Dr. Om Prakash, Professor, UPES ; Dr. Sudhir Joshi, Professor, Graphic Era University & Dr. Yogananda Jeppu, Honeywell Technology Solutions, Hyderabaden_US
dc.identifier.urihttps://dr.ddn.upes.ac.in/handle/123456789/4400
dc.language.isoenen_US
dc.publisherSchool of Advanced Engineering, UPES, Dehradunen_US
dc.subjectThesisen_US
dc.subjectAerospace Engineeringen_US
dc.subjectAirbreathing Hypersonic Modelen_US
dc.subjectFlight Dynamic Simulationen_US
dc.subjectTrim Analysisen_US
dc.subjectBifurcation Analysisen_US
dc.subjectClose Loop Simulationen_US
dc.titleFlight dynamics analysis of generic airbreathing hypersonic vehicle using bifurcation methoden_US
dc.typeThesisen_US

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
Ritesh Singh Thesis SOE.pdf
Size:
9.33 MB
Format:
Adobe Portable Document Format
Description:
Download

License bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
license.txt
Size:
1.71 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

Thesis