Search

list

1 item

full text by request
Compressible Boundary Layer Equations And Stagnation Point Solution With Differences In Thermal And Dynamic Boundary Layer Thicknesses Being Considered
Author(s): Buck, Melving L.
Corporate Author(s): Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1961-08
Report number: ASD TR 61-107

Refine your search

Refine your search