Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel /

Bibliographic Details

Corporate Author:	Lewis Research Center
Other Authors:	Johns, Albert L.
Format:	Government Document Book
Language:	English
Published:	[Cleveland, Ohio] : [Lewis Research Center], [1990]
Series:	NASA technical memorandum ; 103258.
Subjects:	Control systems design. Exhaust nozzles. Flow distribution. Flow visualization. High temperature gases. Inlet flow. Laser applications. Nozzle flow. Support systems. Thrust vector control.
Online Access:	https://purl.fdlp.gov/GPO/LPS62061