F-16xl-2 Supersonic Laminar Flow Control Flight Test Experiment

F-16xl-2 Supersonic Laminar Flow Control Flight Test Experiment
Author :
Publisher : Createspace Independent Publishing Platform
Total Pages : 262
Release :
ISBN-10 : 1721931120
ISBN-13 : 9781721931125
Rating : 4/5 (125 Downloads)

Book Synopsis F-16xl-2 Supersonic Laminar Flow Control Flight Test Experiment by : National Aeronautics and Space Administration (NASA)

Download or read book F-16xl-2 Supersonic Laminar Flow Control Flight Test Experiment written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-27 with total page 262 pages. Available in PDF, EPUB and Kindle. Book excerpt: The F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment was part of the NASA High-Speed Research Program. The goal of the experiment was to demonstrate extensive laminar flow, to validate computational fluid dynamics (CFD) codes and design methodology, and to establish laminar flow control design criteria. Topics include the flight test hardware and design, airplane modification, the pressure and suction distributions achieved, the laminar flow achieved, and the data analysis and code correlation. Anders, Scott G. and Fischer, Michael C. Langley Research Center RTOP 537-07-23-21


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Geometrical, flight, computational fluid dynamics (CFD), and wind-tunnel studies for the F-16XL-1 airplane are summarized over a wide range of test conditions.