A Low-Order Aerodynamic Prediction Approach for Fuselage Forces and Wakes.

Simple item page
dc.contributor.advisorAshok Gopalarathnam, Chair
dc.contributor.advisorKenneth Granlund, Member
dc.contributor.advisorGregory Buckner, Member
dc.contributor.authorGupta, Utkarsh Bibhas
dc.date.accepted2017-09-15
dc.date.accessioned2017-10-24T12:33:17Z
dc.date.available2017-10-24T12:33:17Z
dc.date.defense2017-08-15
dc.date.issued2017-08-15
dc.date.released2017-10-24
dc.date.reviewed2017-08-22
dc.date.submitted2017-08-15
dc.degree.disciplineAerospace Engineering
dc.degree.levelthesis
dc.degree.nameMaster of Science
dc.descriptionNorth Carolina State University Theses Mechanical and Aerospace Engineering.
dc.formatM.S. North Carolina State University, 2017.
dc.identifier.otherdeg7205
dc.identifier.urihttp://www.lib.ncsu.edu/resolver/1840.20/34673
dc.rights
dc.titleA Low-Order Aerodynamic Prediction Approach for Fuselage Forces and Wakes.
dcterms.extent1 online resource (xi, 64 pages) : illustrations (some color)

Files

Original bundle

Now showing 1 - 1 of 1
No Thumbnail Available
Name:
etd.pdf
Size:
8.45 MB
Format:
Adobe Portable Document Format
Download

Collections

Theses