THREE-DIMENSIONAL SUPERSONIC FLUTTER MODEL TEST NEAR MACH NUMBER 1.5. PART III. EXPERIMENTAL AND THEORETICAL DATA FOR WINGS WITH CONTROL SURFACES

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1958
Accession Number
AD0118052

Entities

People

  • Gifford W. Asher
  • Warren H. Weatherill

Organizations

  • Massachusetts Institute of Technology

Tags

DTIC Thesaurus Topics

  • Control Surfaces
  • Mach Number
  • Model Tests
  • Physical Properties
  • Surfaces
  • Three Dimensional

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow