A Wing in an Unsteady Gas Flow. Part 2,

Abstract

Contents: Method of the Calculation of Apparent Additional Masses of Wings of Arbitrary Planform; Some Point Solutions; Calculation of the Unsteady Wing Characteristics of Arbitrary Planform; High Subsonic Speeds (0 < M < 1); Method of the Calculation of the Coefficients of Aerodynamic Derivatives; The Velocity Field of Unsteady Discrete Vortex in a Compresses Medium; Method of the Calculation of Aerodynamic Wing Characteristics with Arbitrary Time Dependences; Some Known Solutions; Calculation of the Unsteady Wing Characteristics of Arbitrary Planform; Supersonic Speeds (M > 2); Numerical Method of the Calculation of Aerodynamic Wing Characteristics with Harmonic Time Disturbances; Numerical Method of the Calculation of Aerodynamic Wing Characteristics with Arbitrary Time Dependences; and Some Exact Solutions for Wings with Supersonic Edges with Harmonic Time Dependences.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 08, 1977
Accession Number
ADA049000

Entities

People

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

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamic Characteristics
  • Aerodynamic Forces
  • Aerodynamic Loading
  • Aircrafts
  • Animal Structures
  • Cartesian Coordinates
  • Control Surfaces
  • Coordinate Systems
  • Differential Equations
  • Fluid Dynamics
  • Gas Flow
  • Integral Equations
  • Reliability
  • Self Assembly
  • Sweptback Wings
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Approximation Theory.

Technology Areas

  • Hypersonics