Description:This document describes the design of the leading edge suction system for flight demonstration of hybrid laminar flow control on the Boeing 757 airplane. The exterior pressures on the wing surface and the required suction quantity and distribution were determined in previous work. A system consisting of porous skin, sub-surface spanwise passages ("flutes"), pressure regulating screens and valves, collection fittings, ducts and a turbocompressor was defined to provide the required suction flow. Provisions were also made for flexible control of suction distribution and quantity for HLFC research purposes. Analysis methods for determining pressure drops and flow for transpiration heating for thermal anti-icing are defined. The control scheme used to observe and modulate suction distribution in flight is described. Langley Research Center NAS1-18574; RTOP 522-32-31-01We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with High Reynolds Number Hybrid Laminar Flow Control (Hlfc) Flight Experiment. Report 4; Suction System Design and Manufacture. To get started finding High Reynolds Number Hybrid Laminar Flow Control (Hlfc) Flight Experiment. Report 4; Suction System Design and Manufacture, you are right to find our website which has a comprehensive collection of manuals listed. Our library is the biggest of these that have literally hundreds of thousands of different products represented.
Pages
112
Format
PDF, EPUB & Kindle Edition
Publisher
Createspace Independent Publishing Platform
Release
2018
ISBN
1721078304
High Reynolds Number Hybrid Laminar Flow Control (Hlfc) Flight Experiment. Report 4; Suction System Design and Manufacture
Description: This document describes the design of the leading edge suction system for flight demonstration of hybrid laminar flow control on the Boeing 757 airplane. The exterior pressures on the wing surface and the required suction quantity and distribution were determined in previous work. A system consisting of porous skin, sub-surface spanwise passages ("flutes"), pressure regulating screens and valves, collection fittings, ducts and a turbocompressor was defined to provide the required suction flow. Provisions were also made for flexible control of suction distribution and quantity for HLFC research purposes. Analysis methods for determining pressure drops and flow for transpiration heating for thermal anti-icing are defined. The control scheme used to observe and modulate suction distribution in flight is described. Langley Research Center NAS1-18574; RTOP 522-32-31-01We have made it easy for you to find a PDF Ebooks without any digging. And by having access to our ebooks online or by storing it on your computer, you have convenient answers with High Reynolds Number Hybrid Laminar Flow Control (Hlfc) Flight Experiment. Report 4; Suction System Design and Manufacture. To get started finding High Reynolds Number Hybrid Laminar Flow Control (Hlfc) Flight Experiment. Report 4; Suction System Design and Manufacture, you are right to find our website which has a comprehensive collection of manuals listed. Our library is the biggest of these that have literally hundreds of thousands of different products represented.