FORCE AND PRESSURE RECOVERY CHARACTERISTICS AT SUPERSONIC SPEEDS OF A CONICAL SPIKE INLET WITH A BYPASS DISCHARGING FROM THE TOP OR BOTTOM OF THE DIFFUSER IN AN AXIAL DIRECTION

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 23, 1953
Accession Number
AD0005016

Entities

People

  • Andrew Beke
  • J. L. Allen

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Additives (Chemicals)
  • Boundary Layer
  • Combustion Chambers
  • Diffusers
  • Dynamic Pressure
  • Engines
  • Flow
  • Flow Fields
  • Free Stream
  • Jet Engines
  • Leading Edges
  • Mach Number
  • Mass Flow
  • Measurement
  • Static Pressure
  • Subsonic Diffusers
  • Turbojet Engines

Technology Areas

  • Hypersonics