scispace - formally typeset
A

Alejandra Uranga

Researcher at University of Southern California

Publications -  27
Citations -  749

Alejandra Uranga is an academic researcher from University of Southern California. The author has contributed to research in topics: Boundary layer & Propulsion. The author has an hindex of 9, co-authored 25 publications receiving 534 citations. Previous affiliations of Alejandra Uranga include Massachusetts Institute of Technology & Florida Institute of Technology.

Papers
More filters
Journal ArticleDOI

Implicit Large Eddy Simulation of transition to turbulence at low Reynolds numbers using a Discontinuous Galerkin method

TL;DR: In this paper, the authors predict the formation of laminar separation bubbles at low Reynolds numbers and the related transition to turbulence by means of Implicit Large Eddy Simulations with a high-order Discontinuous Galerkin method.
Journal ArticleDOI

Boundary layer ingestion propulsion benefit for transport aircraft

TL;DR: In this article, the physical principles of aerodynamic power savings from boundary layer ingestion propulsion and a quantitative evaluation of the boundary-layer ingestion bene... are presented. But they do not consider the impact of boundary layer insertion on the propulsion system.
Proceedings ArticleDOI

Preliminary Experimental Assessment of the Boundary Layer Ingestion Benefit for the D8 Aircraft

TL;DR: In this article, the aerodynamic benefit of boundary layer ingestion (BLI) for the D8 transport aircraft concept was evaluated in the NASA Langley 14⇥22 Foot Subsonic Wind Tunnel and the results showed that the model BLI propulsors require 6% less electrical power at simulated cruise point.
Journal ArticleDOI

Boundary Layer Ingestion Benefit of the D8 Transport Aircraft

TL;DR: In this article, the authors present the experimental assessment of the aerodynamic benefit of boundary layer ingestion for an advanced design civil transport aircraft, the D8 "double bubble", carried out from 2010 to 2013.
Journal ArticleDOI

Analysis of the Aerodynamic Benefit from Boundary Layer Ingestion for Transport Aircraft

TL;DR: In this paper, boundary layer ingestion (BLI) was used to generate a propulsive force with lower flow power input than conventional engines, and the aerodynamic benefit can be traced back to its sources: reducti...