Simulate the SUI Endurance Drone!​

​

​

​

​

​

 

 

 

Conditions

Calculations should be performed for

validation against existing experimental measurements as documented in NASA TM—2018–219758.

Suggested cases are listed below:

​​​

​

Case                                      Run           Test Points      Type                                                             
Isolated Fuselage               118            5 - 15                20 ft/s Pitch Sweep

Isolated Rotor Hover         26              4 - 9                  Hover RPM Sweep

Full Vehicle                          119            4 - 15                Hover RPM Sweep

Full Vehicle                          104            31                     20 ft/s, -4.98° pitch, differential rotors

 

CAD for the SUI Endurance is available on the file share page.

​

​​

NASA WT Reference:

​

​