THEORETICAL STUDIES ON THE PREDICTION OF UNSTEADY SUPERSONIC AIRLOADS ON ELASTIC WINGS. PART 2. RULES FOR APPLICATION OF OSCILLATORY SUPERSONIC AERODYNAMIC INFLUENCE COEFFICIENTS

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1956
Accession Number
AD0110592

Entities

People

  • Garabed Zartarian

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Bibliographies
  • Boundaries
  • Deflection
  • Delta Wings
  • Downwash
  • Grids
  • Interpolation
  • Leading Edges
  • Mach Number
  • Steady State
  • Trailing Edges
  • United States

Technology Areas

  • Hypersonics