INVESTIGATION OF JET EFFECTS ON A FLAT SURFACE DOWNSTREAM OF THE EXIT OF A SIMULATED TURBOJET NACELLE AT A FREE-STREAM MACH NUMBER OF 1.39

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Document Details

Document Type
Technical Report
Publication Date
Apr 02, 1956
Accession Number
AD0093276

Entities

People

  • Abraham Leiss
  • Walter E. Bressette

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Convergent Divergent Nozzles
  • Exhaust Gases
  • Flow
  • Free Stream
  • Government Procurement
  • Governments
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Shock Waves
  • Static Pressure
  • Surface Properties
  • Trailing Edges
  • Turbojet Engines
  • United States Government
  • Unmanned Aerial Vehicles