Investigation of bellows and flex hose induced vibrations in spacecraft ducting components
Minimum pressure loss in high velocity flow duct systems
1971-04-28
Miscellaneous
No indication
English
Design and qualification testing of high-pressure, high-velocity aircraft duct systems
Engineering Index Backfile | 1957
|Flow and Loss Mechanisms Within an Interturbine Duct
AIAA | 2016
|Flow and Loss Mechanisms Within an Interturbine Duct
Online Contents | 2016
|