Loading...
A Study at a Mach Number of 2.01 of the Shock Boundary-Layer Interaction Resulting from the Deflection of a Wedge Mounted on a Bypass Plate
Landrum, Emma Jean
Landrum, Emma Jean
Abstract
Description
Date
1961
Journal Title
Journal ISSN
Volume Title
Publisher
Collections
Download Dataset
Files
Loading...
10614827.pdf
Adobe PDF, 2.07 MB
Rights Holder
Usage License
Embargo
Research Projects
Organizational Units
Journal Issue
Keywords
Citation
Advisor
Department
Physics
DOI
https://dx.doi.org/doi:10.21220/s2-8hw9-hh54