A Physics-Based Approach to Urban Air MobilityHigh-fidelity Computational Fluid Dynamics (CFD) simulations for multi-rotor vehicles have been carried out. The three-dimensional unsteady Navier-Stokes equations are solved on overset grids employing high order accurate schemes, dual-time stepping, and a hybrid turbulence model using NASA's CFD code Over- flow. The vehicles studied consist of small to medium sized drones, and bigger vehicles for future Urban Air Mobility (UAM) applications. The performances for different configurations and rotor mounting are calculated in hover and in forward flight. Understanding the complex flows and the interactions between rotors and with other elements will help design the future multi-rotor vehicles to be quieter, safer, and more efficient.
Document ID
20180007535
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Ventura Diaz, Patricia (Science and Technology Corp. Moffett Field, CA, United States)
Yoon, Steven S. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
November 7, 2018
Publication Date
September 18, 2018
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN60111Report Number: ARC-E-DAA-TN60111
Meeting Information
Meeting: European Rotocraft Forum
Location: Delft
Country: Netherlands
Start Date: September 18, 2018
End Date: September 21, 2018
Sponsors: Council of European Aerospace Societies (CEAS)