The Utilization of the Analytic Graph Method to Determine the Best Shape of Thin Delta Wings in Supersonic Flow,

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Document Details

Document Type
Technical Report
Publication Date
Jun 29, 1978
Accession Number
ADA063773

Entities

People

  • Adriana Nastase
  • C. Nastase
  • Francine Atanasiu-moldovan

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Coefficients
  • Delta Wings
  • Equations
  • Flow
  • Foreign Technology
  • Leading Edges
  • Mach Number
  • Resistance
  • Supersonic Flow
  • Thick Wings
  • Translations

Technology Areas

  • Hypersonics