DETERMINING THE FORM OF A SPATIAL OPTIMUM BODY WITH CONSIDERATION OF FRICTION FORCES (OPREDELENIE FORMY PROSTRANSTVENNOGO OPTIMALNOGO TELA S UCHETOM SILY TRENIYA),

Abstract

The problem of determining the optimum shape of a three-dimensional body in hypersonic flow is considered under the following assumptions: (a) the distribution of pressure coefficients obeys Newton's law; (b) the local friction is constant. This problem is reduced here to two variational problems which consist in determining the extremals of two functionals describing the longitudinal and transverse contours of the body. The two problems are formulated and solved independently, using the Euler equation, with Weierstrass-Erdmann conditions taken into consideration. Some specific limiting cases are investigated which allow simple solutions. The ratio of the total drag of a starlike body in terms of the drag of an equivalent optimal body is given in a graph which shows that a significant reduction in the drag is obtained with a starlike body.

Document Details

Document Type
Technical Report
Publication Date
Oct 06, 1967
Accession Number
AD0676206

Entities

People

  • A. L. Gonor

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Coefficients
  • Drag
  • Equations
  • Euler Equations
  • Flow
  • Friction
  • Hypersonic Flow
  • Mathematics
  • Physical Properties
  • Pressure Distribution
  • Three Dimensional
  • Transverse

Fields of Study

  • Mathematics
  • Physics

Readers

  • Fluid Dynamics.
  • Information Retrieval
  • Operations Research

Technology Areas

  • Hypersonics