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High reynolds number hybrid laminar flow control (hlfc) flight experiment. 3; leading edge design, fabrication, and installation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1999 |
| Description | 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. |
| File Size | 6754937 |
| Page Count | 92 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19990052671 |
| Archival Resource Key | ark:/13960/t2j72cv45 |
| Language | English |
| Publisher Date | 1999-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Suction Flight Tests Laminar Boundary Layer Leading Edge Flaps Laminar Flow Ducts Boeing 757 Aircraft Boundary Layer Control Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |