X-29 ECS High-Alpha Modifications

901221

07/01/1990

Event
International Conference On Environmental Systems
Authors Abstract
Content
It was anticipated that during X-29 extended duration, high angle-of-attack flight (40 to 70 deg), aircraft ECS performance would significantly degrade. Computer modelling of the system indicated that the performance of the ECS decreased as the angle of attack increased. Modifications to improve system performance were analyzed and, as a result of this analysis, ECS hardware modifications have been incorporated on the aircraft. The High-Alpha Flight Test Program has proven the validity of these modifications. To date, the ECS on Ship No. 2 has performed well within its nominal operating parameters in the high-alpha regime.
Meta TagsDetails
DOI
https://doi.org/10.4271/901221
Pages
11
Citation
Amalfitano, M., "X-29 ECS High-Alpha Modifications," SAE Technical Paper 901221, 1990, https://doi.org/10.4271/901221.
Additional Details
Publisher
Published
Jul 1, 1990
Product Code
901221
Content Type
Technical Paper
Language
English