V-22 Flight Test Aerodynamics

VFS-F47-1007

5/6/1991

Authors
Abstract
Content

The status of the aerodynamics and performance of the V-22 Osprey as determined from over 375 hours of flight testing on four aircraft is presented. The data was obtained during envelope expansion where true airspeeds of 280 knots have been achieved in cruise, 349 knots in a dive, and 48,000 pounds of lifting capability has been demonstrated in hover.

Meta TagsDetails
DOI
https://doi.org/10.4050/VFS-F47-1007
Citation
Farrell, M. and Grauer, W., "V-22 Flight Test Aerodynamics," Forum 47 - Phoenix, AZ 1991, Phoenix, AZ, May 6, 1991, https://doi.org/10.4050/VFS-F47-1007.
Additional Details
Publisher
Published
5/6/1991
Product Code
VFS-F47-1007
Content Type
Technical Paper
Language
English