Actions for Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters

Email RIS file
Bookmark
Report an Issue

Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters

Author
Bare, E. Ann
Published
May 1, 1989.
Physical Description
1 electronic document
Additional Creators
Capone, Francis J.
Online Version

Availability

I Want It
I Want It

Finding items...

Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
An investigation was conducted in the Static Test Facility of the Langley 16-Foot Transonic Tunnel to determine the effects of five geometric design parameters on the internal performance of convergent single expansion ramp nozzles. The effects of ramp chordal angle, initial ramp angle, flap angle, flap length, and ramp length were determined. All nozzles tested has a nominally constant throat area and aspect ratio. Static pressure distributions along the centerlines of the ramp and flap were also obtained for each configuration. Nozzle pressure ratio was varied up to 10.0 for all configurations.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19890012397.
Accession ID: 89N21768.
NAS 1.15:4112.
NASA-TM-4112.
L-16535.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15690844