AN INNOVATIVE TECHNIQUE FOR STATIC AND DYNAMIC V/STOL TESTING

VFS-F34-038

5/15/1978

Authors
Abstract
Content

Initial hover testing of the Navy’s XFV-12A V/STOL technology prototype aircraft is being conducted in the former Lunar Lander Research Facility at the NASA Langley Research Center. The aircraft incorporates a unique lift/control concept for V/STOL flight. A key element in the development of this aircraft has been the application of existing hardware and facilities to conserve program funds. Adaptation of the NASA Gantry has created a V/STOL aircraft test facility with unique capability and flexibility. Static lift and control measurements can be obtained and dynamic hover flight can be conducted over a wide range of realistic test conditions.

Meta TagsDetails
DOI
https://doi.org/10.4050/VFS-F34-038
Citation
Culpepper, R., Lewis, E., and Hancock, V., "AN INNOVATIVE TECHNIQUE FOR STATIC AND DYNAMIC V/STOL TESTING," Forum 34 - Washington, D.C. 1978, Washington, D.C., May 15, 1978, https://doi.org/10.4050/VFS-F34-038.
Additional Details
Publisher
Published
5/15/1978
Product Code
VFS-F34-038
Content Type
Technical Paper
Language
English