Shock-Free Configurations in Two- and Three- Dimensional Transonic Flow,

Abstract

An indirect method for finding shock-free airfoils and a nearly direct method for finding shock-free airfoils and wing are discussed. While the mathematics of both procedures is emphasized, illustrative practical results are given. (Author)

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1981
Accession Number
ADA116261

Entities

People

  • A. Robert Seebass

Organizations

  • University of Arizona

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerospace Industry
  • Aircrafts
  • Boundary Layer
  • Boundary Value Problems
  • Computational Fluid Dynamics
  • Computational Science
  • Differential Equations
  • Engineering
  • Equations
  • Flow
  • Fluid Dynamics
  • Mach Number
  • Mechanical Engineering
  • Partial Differential Equations
  • Pressure Distribution
  • Shock Waves
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Approximation Theory.
  • Distributed Systems and Data Platform Development