Bleed Rate Model Based on Prandtl-Meyer Expansion for a Bleed Hole Normal to a Supersonic Freestream

Bleed Rate Model Based on Prandtl-Meyer Expansion for a Bleed Hole Normal to a Supersonic Freestream

Bibliographic Details
Main Author: Bunnag, Shane
Language:English
Published: University of Cincinnati / OhioLINK 2010
Subjects:
Aerospace Materials
boundary layer bleed
Prandtl-Meyer expansion
bleed rate model
shockwave boundary layer interaction
first principles
supersonic inlet
Online Access:http://rave.ohiolink.edu/etdc/view?acc_num=ucin1282330691

Internet

http://rave.ohiolink.edu/etdc/view?acc_num=ucin1282330691

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