Improved hot-film anemometer developed for making high-bandwidth turbulence measurements in moderate-enthalpy supersonic and hypersonic flows (e.g., NASP inlets and control surfaces, HSCT jet exhaust). Features include low thermal inertia, ruggedness, and reduced perturbation of flow.
Microsensor Hot-Film Anemometer
NASA Tech Briefs ; 19 , 4
1995-04-01
Miscellaneous
No indication
English
Microsensor Hot-Film Anemometer
Online Contents | 1995
SPIE | 1994
|Improved Circuit For Hot-Film Anemometer
NTRS | 1993
|British Library Conference Proceedings | 1994
|Hot-Film Anemometer For Boundary-Flow Transitions
NTRS | 1988
|