Experimental Investigation of a 10 degrees Conical Turbojet Plug Nozzle with Translating Primary and Secondary Shrouds at Mach Numbers from 0 to 2.0.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1969
- Accession Number
- ADA956519
Entities
People
- Donald L. Bresnahan
Organizations
- Glenn Research Center