High Reynolds Number Hybrid Laminar Flow Control Hlfc Flight Experiment 3 Leading Edge Design Fabrication And Installation
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High Reynolds Number Hybrid Laminar Flow Control (Hlfc) Flight Experiment. 3; Leading Edge Design, Fabrication, and Installation
Author: National Aeronautics and Space Administration (NASA)
language: en
Publisher: Createspace Independent Publishing Platform
Release Date: 2018-05-31
This document describes the design, fabrication, and installation of the suction panel and the required support structure, ducting, valving, and high-lift system (Krueger flaps) for flight demonstration of hybrid laminar flow control on the Boeing 757 airplane.Langley Research CenterBOUNDARY LAYER CONTROL; LAMINAR BOUNDARY LAYER; LAMINAR FLOW; FLIGHT TESTS; SUCTION; BOEING 757 AIRCRAFT; DUCTS; LEADING EDGE FLAPS
New Results in Numerical and Experimental Fluid Mechanics X
This book presents contributions to the 19th biannual symposium of the German Aerospace Aerodynamics Association (STAB) and the German Society for Aeronautics and Astronautics (DGLR). The individual chapters reflect ongoing research conducted by the STAB members in the field of numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications, and cover both nationally and EC-funded projects. Special emphasis is given to collaborative research projects conducted by German scientists and engineers from universities, research-establishments and industries. By addressing a number of cutting-edge applications, together with the relevant physical and mathematics fundamentals, the book provides readers with a comprehensive overview of the current research work in the field. Though the book’s primary emphasis is on the aerospace context, it also addresses further important applications, e.g. in ground transportation and energy.