Motivation
- Wide range of application for commute and cargo (UAVs, UAMs, e/VTOL (rotary-wing, fixed-wing)
- Operate in urban environment
- Subjected to large disturbances: large wind gusts encounters
- BL characteristics: separated, vortex-dominated, and unsteady flow
- Low speed operation, small aspect ratio, low Reynolds number
- Re: π(104β105)O(10^4-10^5)Γ Poor L/D
Research questions
- What are the underlying physics under unsteady conditions at π π(104β105) Re(10^4-10^5)?
- Is the classical unsteady aerodynamics theory βsmall flow perturbationsβ applicable for flow complex at π π104β105?Re(10^4-10^5 )?
Objective
To advance the aerodynamic performance by the physical understanding of the fluid interactions at π π(104β105) Re(10^4-10^5)
Key results
- Validation: Water-tunnel experiments (In collaboration with AFRL)
- 46x61 cm test section
- πΌπ‘=5 πππsin(ππ‘)Ξ±(t)=5 deg sinβ‘γ(Οtγ)
- π=0.5,π=0.05k=0.5,k=0.05
- π π=2π₯104Re=2x10^4
- Highly unsteady, π π=2Γ104, π=0.5Re=2Γ10^4, k=0.5
- RANS/LES (IDDES)
- Unsteady, π π=2Γ104, π=0.05Re=2Γ10^4, k=0.05
- RANS/LES (IDDES)
- π π=2Γ104 Re=2Γ10^4
- 2D URANS w. transition model
π=0.05k=0.05
π=0.5k=0.5
Read more about the methodology and results in the following publications and proceedings:
- Badrya, C., Govindarajan, B., Medina, A., Yang, S. J., and Chopra, I., Unsteady Aerodynamic Characteristics of Pitching Flat Plates at Low Reynolds Numbers, Journal of Aircraft, Volume 58, Number 4 July 2021, DOI:10.2514/1.C036028
- Catlett, M. R., Anderson J. M, Badrya, C., and Baeder, J. D., Unsteady response of airfoils due to small-scale pitching motion with considerations for foil thickness and wake motion. Journal of Fluids and Structures, Vol.94, 2020. DOI: 10.1016/j.jfluidstructs.2020.102889
- Catlett, M. R., Anderson, J. M., Badrya, C., Govindarajan, B., and Baeder, J. D., Numerical Investigation of Aeroelastic Forces and Pressures on Joukowski Foils of Variable Thickness due to Pitching Motion, 2018 AIAA Aviation, June 2018, Dallas, TX. DOI: 10.2514/6.2018-2906
- Badrya, C., Govindarajan, B., and Chopra, I., Basic Understanding of Unsteady Airfoil Aerodynamics at Low Reynolds Numbers, AIAA Aerospace Sciences Meeting, January 2018, Kissimmee, FL. DOI: 10.2514/6.2018-206