Mission Adaptive Wing Research Programme
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 January 1981
Abstract
Ground testing of representing components is being conducted on the Mission Adaptive Wing (MAW) programme in Seattle, Washington. Phase 2 of a three‐phase wind tunnel programme has been completed and has verified the aerodynamics and loads used for the initial design concept. Unless a major problem is encountered in the ground test programme, a research F‐111 airplane will fly with variable camber wings in August of 1982.
Citation
DeCAMP, R.W. and HARDY, R. (1981), "Mission Adaptive Wing Research Programme", Aircraft Engineering and Aerospace Technology, Vol. 53 No. 1, pp. 10-11. https://doi.org/10.1108/eb035691
Publisher
:MCB UP Ltd
Copyright © 1981, MCB UP Limited