Evolution and Test History of the V-22 0.2-Scale Aeroelastic Model

SM_DYN_1989-2652

11/13/1989

Authors
Abstract
Content

Construction and testing of the V-22 aeroelastic model series occupied a five-year period from mid- 1983 through mid-1988. During this period several variants of the model were subjected to extensive ground testing and 46 weeks of wind tunnel testing during seven entries in three different wind tunnels. The paper discusses model theory and construction techniques plus test plans, purposes, methods, and results.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM_DYN_1989-2652
Citation
Settle, T. and Kidd, D., "Evolution and Test History of the V-22 0.2-Scale Aeroelastic Model," Rotorcraft Dynamics - Arlington, Texas 1989, Arlington, Texas, November 13, 1989, https://doi.org/10.4050/SM_DYN_1989-2652.
Additional Details
Publisher
Published
11/13/1989
Product Code
SM_DYN_1989-2652
Content Type
Technical Paper
Language
English