Accuracy of flat plate, turbulent skin friction at supersonic speeds

Aeronautical Journal

Volumn 104, Issue 1036, 2000, Pages 257-263

  Squire, L C ^a  

^a NONE

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; BOUNDARY LAYERS; COMPRESSIBLE FLOW; DENSITY (SPECIFIC GRAVITY); DRAG; FRICTION; INCOMPRESSIBLE FLOW; INTEGRAL EQUATIONS; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS; TURBULENCE; VISCOSITY;

FLAT PLATE; FLOATING ELEMENT BALANCES; MACH NUMBERS; TURBULENT SKIN FRICTION COEFFICIENT; ZERO PRESSURE GRADIENT;

PLATE METAL;

EID: 0034204648     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (12)

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9. MABEY, D.G. Some observations on the wake component of the velocity profiles of turbulent boundary layers at subsonic and supersonic speeds. Royal Aircraft Establishment Tech Report 77004, 1977.
10. FERNHOLZ, H.H. and FINLEY, P.J. A further compilation of compressible boundary layer data with a survey of turbulence data AGARD Report Ag-263, 1981.
11. GAUDET, L. Experimental investigation of the turbulent boundary layer at High Reynolds numbers and a Mach number of 0·8. Royal Aircraft Establishment Tech Report 84094, 1984.
12. FERNHOLZ, H.H. and FINLEY, P.J. A critical commentary on mean flow data for two-dimensional compressible turbulent boundary layers. AGARD Report Ag-253, 1980.