A Wing in an Unsteady Gas Flow. Part 3,

Abstract

Contents: Some Precise Solutions for Wings with Supersonic Edges with Arbitrary Time Dependences; Procedure of Calculation of the Aerodynamic Wing Characteristics of Arbitrary Planform; Practical Applications; Special Features of the Practical Use of Duhamel Integral in Tasks of Aerodynamics; Approximation Method; Coefficients of the Aerodynamic Derivative and of Apparent Additional Masses; Some Common Properties of Unsteady Effect of Planform, Numbers M and p* on the Aerodynamic Derivatives of Wings; and Effect of Planform, the Mach Numbers and Laws of Motion for Transient Functions.

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Document Details

Document Type
Technical Report
Publication Date
Sep 08, 1977
Accession Number
ADA049001

Entities

People

  • B. K. Skripach
  • S. M. Belotserkovskiy
  • V. G. Tabachnikov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Loading
  • Aerodynamics
  • Aeroelasticity
  • Aircraft Equipment
  • Aircrafts
  • Computational Science
  • Delta Wings
  • Fluid Dynamics
  • Fluid Flow
  • Gas Flow
  • Hydrodynamics
  • Mach Number
  • Mechanics
  • Sweptback Wings
  • Time Dependence
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics