NDLI: Low-speed aerodynamic investigations of a hybrid wing body configuration

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Low-speed aerodynamic investigations of a hybrid wing body configuration

Content Provider	NASA Technical Reports Server (NTRS)
Author	Vicroy, Dan D. Gatlin, Gregory M. Jenkins, Luther N. Carter, Melissa B. Murphy, Patrick C.
Copyright Year	2014
Description	Two low-speed static wind tunnel tests and a water tunnel static and dynamic forced-motion test have been conducted on a hybrid wing-body (HWB) twinjet configuration. These tests, in addition to computational fluid dynamics (CFD) analysis, have provided a comprehensive dataset of the low-speed aerodynamic characteristics of this nonproprietary configuration. In addition to force and moment measurements, the tests included surface pressures, flow visualization, and off-body particle image velocimetry measurements. This paper will summarize the results of these tests and highlight the data that is available for code comparison or additional analysis.
File Size	2929789
Page Count	16
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20150000554
Archival Resource Key	ark:/13960/t57d7w84d
Language	English
Publisher Date	2014-06-16
Access Restriction	Open
Subject Keyword	Aerodynamics Aircraft Design, Testing And Performance Pitching Moments Body-wing Configurations Computational Fluid Dynamics Low Speed Aerodynamic Coefficients Wing Nacelle Configurations Water Tunnel Tests Navier-stokes Equation Subsonic Wind Tunnels Contours Wind Tunnel Tests Flow Visualization Investigation Flow Velocity Particle Image Velocimetry Cruising Flight Hydraulic Test Tunnels Angle of Attack Aerodynamic Characteristics Leading Edges Hybrid Structures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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