WebBy ingesting and reenergizing the boundary layer flow, BLI reduces by 40% in the D8 the wasted kinetic energy in the combined high-velocity jet exhaust and slow-speed wake behind the fuselage. Large-scale wind-tunnel testing with NASA showed a power-saving from BLI from 8.4% with the same jet nozzle area to 10.4% with the same mass flow. The ... WebMar 13, 2024 · Embedded boundary layer ingestion propulsion systems can also enable nacelles with reduced surface area and associated weight and drag, further decreasing the aircraft propulsive power requirement. The required propulsor flow power is shown to decrease with increases in both the amount of boundary layer ingested and the …
Aeromechanical Response of a Distortion-Tolerant Boundary Layer ...
WebJun 9, 2024 · A key priority for NASA Aeronautics is investing in electrified aircraft propulsion (EAP) technologies for their potential to reduce fuel consumption, emissions, and noise for commercial airplanes. ... where an all-electric propulsor takes advantage of an aerodynamic benefit known as boundary layer ingestion (BLI). The idea behind BLI is … WebJan 1, 2001 · A study is being conducted to improve the propulsion/airframe integration for the Blended Wing-Body (BWB) configuration with boundary layer ingestion nacelles. TWO unstructured grid flow solvers, USM3D and FUN3D, have been coupled with different design methods and are being used to redesign the aft wing region and the nacelles to reduce … make a chess board out of wood
Aurora D8 - Wikipedia
WebJan 9, 2024 · Airframe-propulsion integration concepts that use boundary layer ingestion have the potential to reduce aircraft fuel burn. One concept that has been recently … WebSep 30, 2024 · Propulsors with boundary layer ingestion (BLI) generate a propulsive force with lower flow power input than conventional engines. This aerodynamic benefit can be traced back to its sources: reductions in jet, surface, and wake dissipation. A framework for BLI analysis is developed based on the power balance method: parametric expressions … WebNASA SBIR 2024-II Solicitation. Proposal Summary. Proposal Information. Proposal Number: 22-2- A1.02-1831. Phase 1 Contract #: 80NSSC22PB055. Subtopic Title: Quiet Performance - Aircraft Propulsion Noise. Proposal Title: Advanced Phased Array Instrumentation and Processing for Engine Inlet Measurements. Small Business Concern ... make a chembuster uk