DETERMINATION OF THE EXTERNAL CONTOUR OF A BODY OF REVOLUTION WITH A CENTRAL DUCT SO AS TO GIVE MINIMUM DRAG IN SUPERSONIC FLOW, WITH VARIOUS PERIMETRAL CONDITIONS IMPOSED UPON THE MISSILE GEOMETRY. PART III. NUMERICAL APPLICATION

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1953
Accession Number
AD0030346

Entities

People

  • Carlo Ferrari

Organizations

  • Calspan

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Cartesian Coordinates
  • Coefficients
  • Equations
  • Errors
  • Flow
  • Free Stream
  • Fresnel Integrals
  • Geometry
  • Government Procurement
  • Integral Equations
  • Integrals
  • Radial Velocity
  • Simultaneous Equations
  • Supersonic Flow
  • Three Dimensional
  • Two Dimensional

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow