Flight Data Reduction of Wake Velocity Measurements Using an Instrumented OV-10 Airplane
Flight Data Reduction of Wake Velocity Measurements Using an Instrumented OV-10 Airplane
- New search for: Vicroy, Dan D.
- New search for: Stuever, Robert A.
- New search for: Stewart, Eric C.
- New search for: Rivers, Robert A.
- New search for: Vicroy, Dan D.
- New search for: Stuever, Robert A.
- New search for: Stewart, Eric C.
- New search for: Rivers, Robert A.
A series of flight tests to measure the wake of a Lockheed C- 130 airplane and the accompanying atmospheric state have been conducted. A specially instrumented North American Rockwell OV-10 airplane was used to measure the wake and atmospheric conditions. An integrated database has been compiled for wake characterization and validation of wake vortex computational models. This paper describes the wake- measurement flight-data reduction process.
Document information
Flight Data Reduction of Wake Velocity Measurements Using an Instrumented OV-10 Airplane
1999-09-01
Report
No indication
English
Similar titles
LDA System for In-Flight Local Velocity Measurements on Airplane Wings
| British Library Conference Proceedings | 1999
Flight measurements of velocity distribution and persistence of trailing vortices of airplane
| Engineering Index Backfile | 1955
The effect of flight path inclination on airplane velocity
| Engineering Index Backfile | 1926