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

Author

Emma Jean Landrum, College of William & Mary - Arts & Sciences

Date Awarded

1961

Document Type

Thesis

Degree Name

Master of Arts (M.A.)

Department

Physics

DOI

https://dx.doi.org/doi:10.21220/s2-8hw9-hh54

Rights

© The Author

Recommended Citation

Landrum, Emma Jean, "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" (1961). Dissertations, Theses, and Masters Projects. William & Mary. Paper 1539624525.
https://dx.doi.org/doi:10.21220/s2-8hw9-hh54