NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Performance Characteristics of Cylindrical Target-type Thrust ReversersFrom tests on cylindrical target-type thrust reversers, it was found that the reverser frontal area, lip angle, end-plate angle, and end-plate depth had important effects on reverse-thrust performance. Frontal area, reverser depth, lip angle, and end-plate angele had important effects on the spacing required for unrestricted nozzle flow. For reverse-thrust ratios greater than 64 percent, the reversed flow attached to the 7 degree cowl in quiescent air. Swept-type cylindrical reversers were generally unstable. The thrust-modulation characteristics of a cylindrical target-type thrust reverser were found to be satisfactory.
Document ID
19930088944
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Steffen, Fred W
Mcardle, Jack G
Date Acquired
August 16, 2013
Publication Date
January 11, 1956
Report/Patent Number
NACA-RM-E55I29
Accession Number
93R18234
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available