_____________

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

Custom Designs

Model Support

Force Balances

Class Experiments

Installations

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All Products

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Programming

LabVIEW

Real-Time

Man-in-the-Loop

HW-in-the-Loop

 

 

Rolling Hills Research Corporation

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F/A-18 Test

Normal Force Coefficient for an F/A-18 During Angle of Attack Sweep at Zero Sideslip

F/A-18 Dynamic Test

Normal Force Coefficient for an F/A-18 Undergoing Pitching Motion

a = 15 to 55 to 15

 

 

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