An 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
Correlation of Flight-Test Loads with Wind- Tunnel Predicted Loads on Three Lifting Body Vehicles
NASA Symposium on Flight Test Results Pertaining to the Space Shuttlecraft ; 1970 ; Edwards, CA, US
1970-10-01
Conference paper
No indication
English
Wind tunnel virtual flight test system for lifting body model
European Patent Office | 2021
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