This viewgraph document reviews NASA Dryden's work on Aerial refueling, with specific interest in calculating the drag of the refueling system. The aerodynamic drag of an aerial refueling assembly was calculated during the Automated Aerial Refueling project at the NASA Dryden Flight Research Center. An F/A-18A airplane was specially instrumented to obtain accurate fuel flow measurements and to determine engine thrust
Calculated Drag of an Aerial Refueling Assembly Through Airplane Performance Analysis
2004
29 pages
Report
Keine Angabe
Englisch
CALCULATED DRAG OF AN AERIAL REFUELING ASSEMBLY THROUGH AIRPLANE PERFORMANCE ANALYSIS
British Library Conference Proceedings | 2004
|