Lifting Bodies Derived from Supersonic Flows Past Inclined Circular and Elliptic Cones

Abstract

Lifting-body configurations are constructed from stream surfaces generated by means of supersonic flows past inclined circular and elliptic cones. By such means waverider shapes are devised with curved surfaces and known pressure fields and shock-layer structures. The conical flow fields stem from perturbations of the basic axisymmetric cone flow arising from small angle of attack and small cross-section eccentricity. The approximate results are analytic and in the form of hypersonic small disturbance theory. Various possibilities for waverider shapes are discussed. Design formulas are presented that determine how the Mach number, angle of attack, cross-section eccentricity, and characteristic cone angle affect the waverider shape, pressure distribution, and shock-layer structure.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1978
Accession Number
ADA068003

Entities

People

  • Maurice L. Rasmussen

Organizations

  • University of Oklahoma

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Aircrafts
  • Boundary Layer
  • Control Surfaces
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Fluid Mechanics
  • Geometry
  • Lifting Bodies
  • Mach Number
  • Pressure Distribution
  • Shape
  • Stratified Fluids
  • Supersonic Flow
  • Symmetry

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Structural Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow