Accession Number : AD0697900

Title :   EFFECT OF AIRFOIL SHAPE ON THE AERODYNAMIC CHARACTERISTICS OF A WING NEAR A GROUND-PLATE SURFACE.

Descriptive Note : R. E. Gibson Library bulletin translation series,

Corporate Author : JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB

Personal Author(s) : Yukhimenko,A. I.

Report Date : 18 SEP 1969

Pagination or Media Count : 15

Abstract : Considered is the two-dimensional problem of motion of a slender wing in a potential fluid flow at small distances from a solid ground-plate, which corresponds to the case of high-speed motion of a wing above the interface between two fluids of different density. The problem is solved under the assumption that the fluid is ideal and incompressible, the motion outside the wing is potential, the wing is slender, and the angles of attack are small. (Author)

Descriptors :   (*WINGS, *GROUND EFFECT), AERODYNAMIC CONFIGURATIONS, AERODYNAMIC CHARACTERISTICS, NUMERICAL ANALYSIS, ONE DIMENSIONAL FLOW, SLENDER BODIES, INTERFACES, INCOMPRESSIBLE FLOW, ANGLE OF ATTACK, USSR

Subject Categories : Aerodynamics
      Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE