Inviscid Flow Analysis on Body of Revolution with Slender Cruciform Canted Delta Fins at Small Angle of Incidence.

Abstract

An analysis of the aerodynamic characteristics for a slender fin-body configuration at transonic speeds with an exhaust plume has been developed. Sample calculations for small combined angles of attack, yaw and fin cant, are presented. The analysis is limited to cases of subsonic fin leading edges.

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1975
Accession Number
ADA012770

Entities

People

  • Jingen Wu
  • N. Uchiyama

Organizations

  • University of Tennessee Space Institute

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Angle Of Incidence
  • Exhaust Plumes
  • Flow
  • Inviscid Flow
  • Leading Edges
  • Plumes
  • Revolutions

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.