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Accession Number AD-882 075/5
Title Two-Dimensional Transonic Wind Tunnel Tests of Three 15-Percent Thick Circulation Control Airfoils.
Publication Date Dec 1970
Media Count 72p
Personal Author R. J. Englar
Abstract Two-dimensional transonic wind tunnel tests were conducted on three fifteen percent circulation control elliptic airfoils over the Mach no. range 0.3 to 0.9. Model configurations included a pure elliptical shape with both jet flap and tangential upper sur ...
Keywords Airfoils
Coanda effect
Drag
Jet flaps
Lift
Subsonic characteristics
Trailing edge
Two dimensional flow
 
Source Agency Non Paid Delimited ADS
NTIS Subject Category 46B - Fluid Mechanics
Corporate Author Naval Ship Research and Development Center Washington D C Aviation Dept
Document Type Technical report
Title Note Technical note.
NTIS Issue Number 7622
Contract Number N/A

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