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

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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

Author(s):
Yukhimenko, A. I.
Author Organization(s):
JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Descriptive Note:
R. E. Gibson Library bulletin translation series,
Supplementary Note:
Trans. of Gidrodinamika Bolshikh Skorostei (USSR) n2 p34-46 1966, by L. J. Holtschlag.
Annotation:
Effect of airfoil shape on the aerodynamic characteristics of a wing near a ground-plate surface--Translation.
Pagination:
0015

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
APL-CLB-3-T-603
Contract/Grant Number(s):
NOw-62-0604
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*WINGS, *GROUND EFFECT), AERODYNAMIC CONFIGURATIONS, AERODYNAMIC CHARACTERISTICS, NUMERICAL ANALYSIS, ONE DIMENSIONAL FLOW, SLENDER BODIES, INTERFACES, INCOMPRESSIBLE FLOW, ANGLE OF ATTACK, USSR
Field(s)/Group(s):
Aerodynamics, Aircraft, Fluid Mechanics
Keyword(s):
TRANSLATIONS
Report Date:
1969 Sep 18