Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds

Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds
Author :
Publisher :
Total Pages : 170
Release :
ISBN-10 : NASA:31769000474612
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds by : John E. Lamar

Download or read book Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds written by John E. Lamar and published by . This book was released on 2001 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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. Details are as follows: (1) For geometry, the upper surface of the airplane and the numerical surface description compare reasonably well. (2) For flight, CFD, and wind-tunnel surface pressures, the comparisons are generally good at low angles of attack at both subsonic and transonic speeds; however, local differences are present. In addition, the shock location at transonic speeds from wind-tunnel presure contours is near the aileron hinge line and generally is in correlative agreement with flight results.


Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds Related Books

Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds
Language: en
Pages: 170
Authors: John E. Lamar
Categories: Airplanes
Type: BOOK - Published: 2001 - Publisher:

DOWNLOAD EBOOK

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.
Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16xl-1) at Subsonic and Transonic Speeds
Language: en
Pages: 168
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-06-15 - Publisher: Createspace Independent Publishing Platform

DOWNLOAD EBOOK

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.
NASA Technical Paper
Language: en
Pages: 170
Authors:
Categories: Science
Type: BOOK - Published: - Publisher:

DOWNLOAD EBOOK

Innovation in Flight
Language: en
Pages: 406
Authors: Joseph R. Chambers
Categories: Aeronautics
Type: BOOK - Published: 2005 - Publisher:

DOWNLOAD EBOOK

Monthly Catalog of United States Government Publications
Language: en
Pages: 636
Authors:
Categories: Government publications
Type: BOOK - Published: 2003 - Publisher:

DOWNLOAD EBOOK