Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0
Overview & Synopsis
Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle designed for flight Mach numbers to 3.0
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(
ntrs.nasa.gov)
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Document Information
| Document Title | Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 |
|---|---|
| Author / Organization | Mihaloew, J. R., Stofan, A. J. |
| Subject & Discipline | TECHNICAL_MEMORANDUM |
| Categories | Aerospace & Aviation |
| Publication Year | 2019 |
| License / Rights | Public Domain / NASA STI Open Access |
| Resource Verification | Listed PDF (Verification Pending) |
| Original Host Website |
NASA Technical Reports Server
(ntrs.nasa.gov)
|
| File Format | application/pdf (Portable Document Format) |
| Language | EN |
| Catalog ID | DOC-80525 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |