- Author
-
Hill, R.
- Title
- Feasibility of Detecting a Burner-Can Burn-Through by Means ofCO, CO2, Pressure, and Air Temperature Levels in a Jet Engine Nacelle. Final Report. January 1972-July 1973.
- Coporate
- Federal Aviation Administration, Atlantic City, NJ
- Sponsor
- Federal Aviation Administration, Washington, DC
- Report
-
FAA-RD-74-18,
March 1974,
25 p.
- Distribution
- Available from National Technical Information Service
- Contract
- FAA-181-522-010
- Keywords
-
jet engines
|
nacelle fires
|
combustion chambers
|
supersonic aircraft
|
carbon monoxide
|
carbon dioxide
|
pressure
|
air temperature
|
tests
- Identifiers
- thermal failure (burn-through); engine case rupture containment; structural damage