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The ''delta p'' approach from nike combustion instability
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1965 |
| Description | Applicability of delta p approach to study of combustion instability in liquid and solid propellant rocket engines |
| File Size | 479316 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660026016 |
| Archival Resource Key | ark:/13960/t0dv68p8j |
| Language | English |
| Publisher Date | 1965-10-04 |
| Access Restriction | Open |
| Subject Keyword | Stagnation Flow Solid Propellant Rocket Engine Liquid Propellant Rocket Engine Combustion Instability Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |