A Wing in an Unsteady Gas Flow. Part 1,
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 08, 1977
- Accession Number
- ADA048999
Entities
People
- B. K. Skripach
- S. M. Belotserkovskiy
- V. G. Tabachnikov
Organizations
- National Air and Space Intelligence Center