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Correlation of flight-test loads with wind- tunnel predicted loads on three lifting body vehiclesAn essential area of research with the unique M2-F2, HL-10, and X-24A lifting body configurations is the assessment of the ability to predict flight loads from wind- tunnel tests. Flight measurements and correlation with predictions are necessary in verifying the structural integrity of existing vehicles and establishing the groundwork for weight savings on future vehicles of similar shapes.

As part of the overall lifting body flight investigation at the Flight Research Center, detailed aerodynamic-load studies are being made on each of the three vehicles. This paper presents the preliminary results from these studies
Document ID
19710000632
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Ming H Tang
(Flight Research Center Rosamond, California, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1970
Publication Information
Publication: Flight Test Results Pertaining to the Space Shuttlecraft
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: NASA Symposium on Flight Test Results Pertaining to the Space Shuttlecraft
Location: Edwards, CA
Country: US
Start Date: June 30, 1970
Sponsors: Flight Research Center
Accession Number
71N10106
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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