|
_____________
Aero Research
 Summary
Boundary
Layer
Non-Linear
Aero
Drag
Reduction
Forebody
Vortex
Enhanced
NLF
Helicopter
Blade
Model
Fabrication
LabVIEW Programs
Research
Papers
_____________
Water Tunnels
Summary
Model
2436
Model
1520
Model
0710
Model
2403
Model
Support
Force
Balances
Class
Experiments
Installations
_____________
All
Products
_____________
Programming
LabVIEW
Real-Time
Man-in-the-Loop
HW-in-the-Loop
Rolling Hills Research Corporation
Copyright @2007
All Rights Reserved
| |
|
Normal
Force Coefficient for an F/A-18 During Angle of Attack Sweep at Zero
Sideslip
Normal
Force Coefficient for an F/A-18 Undergoing Pitching Motion
a = 15°
to 55° to 15°
|
|
