EFFECTS OF EXHAUST NOZZLE RECOMBINATION ON HYPERSONIC RAMJET PERFORMANCE. I - EXPERIMENTAL MEASUREMENTS
Overview & Synopsis
Temperature measurements in supersonic nozzles for hydrogen-air and methane-air combustion products at stagnation temperatures up to 5,400 degrees rankine and pressures up to 4.5 atmospheres
Indexed from repository: NASA Technical Reports Server
(
ntrs.nasa.gov)
Document Information
| Document Title | EFFECTS OF EXHAUST NOZZLE RECOMBINATION ON HYPERSONIC RAMJET PERFORMANCE. I - EXPERIMENTAL MEASUREMENTS |
|---|---|
| Author / Organization | Franciscus, L. C., Lezberg, E. A. |
| Subject & Discipline | REPRINT |
| Categories | Aerospace & Aviation |
| Publication Year | 2011 |
| 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-74921 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |