JET EFFECTS ON CYLINDRICAL AFTERBODIES HOUSING SONIC AND SUPERSONIC NOZZLES WHICH EXHAUST AGAINST A SUPERSONIC STREAM AT ANGLES OF ATTACK FROM 90 DEGREES TO 180 DEGREES

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1962
Accession Number
AD0273312

Entities

People

  • Lovick O. Jr. Hayman
  • Russell W. Mcdearmon

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Afterbodies
  • Supersonic Nozzles

Technology Areas

  • Hypersonics