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Ragsdale, William C.

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1.
An experimental investigation of the laminar boundary layer on a spinning ogive cylinder in supersonic flow
Author
Ragsdale, William C.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
2.
Flow field measurements around an ogive-cylinder at angles of attack up to 15 degrees for mach numbers 3.5 and 4
Author
Ragsdale, William C.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
3.
Flow visualization workshop report
Author
Ragsdale, William C.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online