Accession Number:

ADA048999

Title:

A Wing in an Unsteady Gas Flow. Part 1,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1977-09-08

Pagination or Media Count:

517.0

Abstract:

Contents Aerodynamic Coefficients Formulation of the Problem of the Unsteady Motion of Wing Basic Formula for the Potential of the Disturbed Velocities Common Properties of Linear Unsteady Problems, and Similarity Parameters Duhamel Integral, Theorem of Momentum, and Rational Method of Solution of Linear Unsteady Problems Reciprocity Theorem and Its Corollaries Experimental Determination of Unsteady Aerodynamic Wing Characteristics Low Speeds Incompressible Medium M 0 The Velocity Field of Oblique Horseshoe Vortex in an Incompressible Medium Method of the Calculation of Aerodynamic Wing Characteristics with the Harmonic Dependences of the Kinematic Parameters on Time and Method of the Calculation of Aerodynamic Wing Characteristics with the Arbitrary Dependences of the Kinematic Parameters on Time.

Subject Categories:

  • Aircraft
  • Numerical Mathematics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE