1. DSpace at UPES
  2. Knowledge Repository by Schools
  3. School of Engineering
  4. Thesis
Please use this identifier to cite or link to this item: https://dr.ddn.upes.ac.in//xmlui/handle/123456789/4400
Full metadata record
DC FieldValueLanguage
dc.contributor.authorSingh, Ritesh-
dc.date.accessioned2025-02-04T12:03:57Z-
dc.date.available2025-02-04T12:03:57Z-
dc.date.issued2024-03-
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//xmlui/handle/123456789/4400-
dc.descriptionThesis submitted in partial fulfillment of the requirements for the award of the Degree of Doctor of Philosophy (Aerospace Engineering)en_US
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
Appears in Collections:Thesis

Files in This Item:
File Description SizeFormat 
Ritesh Singh Thesis SOE.pdf9.56 MBAdobe PDFView/Open
Show simple item record


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.