SUPERSONIC-AREA-RULE DESIGN AND ROCKET-PROPELLED FLIGHT INVESTIGATION OF A ZERO-LIFT STRAIGHT-WING-BODY-NACELLE CONFIGURATION BETWEEN MACH NUMBERS 0.8 AND 1.53

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Document Details

Document Type
Technical Report
Publication Date
Apr 26, 1956
Accession Number
AD0093071

Entities

People

  • Sherwood Hoffman

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aspect Ratio
  • Bodies
  • Bodies Of Revolution
  • Drag
  • Fineness Ratio
  • Friction
  • Government Procurement
  • Governments
  • Mach Number
  • Measurement
  • Moment Of Inertia
  • Parabolic Bodies
  • Peak Values
  • Reynolds Number
  • United States Government
  • Wing Body Configurations

Technology Areas

  • Hypersonics