J58/YF-12 Ejector Nozzle Performance

740832

02/01/1974

Event
Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
The Lockheed YF-12 aircraft uses a blow-in door ejector nozzle, which consists of a variable area, primary nozzle mounted on the afterburner of a Pratt & Whitney Aircraft J58 engine and blow-in doors, a convergent-divergent spool piece, and variable exit area free-floating flaps integrated into a Lockheed YF-12 airframe. Performance data from cold-flow, wind tunnel models and hot-flow, static stand models were correlated and compared with actual flight test data. It was found that these data showed agreement when both internal thermodynamic and external aerodynamic effects were considered.
Meta TagsDetails
DOI
https://doi.org/10.4271/740832
Pages
11
Citation
Herrick, P., "J58/YF-12 Ejector Nozzle Performance," SAE Technical Paper 740832, 1974, https://doi.org/10.4271/740832.
Additional Details
Publisher
Published
Feb 1, 1974
Product Code
740832
Content Type
Technical Paper
Language
English