Investigation of bellows and flex hose induced vibrations in spacecraft ducting components
Minimum pressure loss in high velocity flow duct systems
28.04.1971
Sonstige
Keine Angabe
Englisch
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
|