Coanda Effect References

"Development of Circulation Control Technology for Application to Advanced Subsonic Transport Aircraft", RJ Englar, MJ Smith, SM Kelley, RC Rover AIAA 93-0644.

US Patent 4,579,300 Internal Wing Aircraft

US Patent 4,568,042 Internal Wing Aircraft

"Steam Fires Underwater Jet Engine", New Scientist, 1st March 2003, P19

"Drive Like the Wind", New Scientist, 9th June 2001

Development of the A6 Circulation Control Wing Flight Demonstrator Configuration, RJ Englar, DTNSRDC ASED 79-01

Applications of the Coanda Effect, Imants Reba, Scientific American, June 1966

The Coanda Effect, GH Stine, Analog Science Fiction/ Science Fact, 1974

X Wing:  A New Concept in Rotry Wing VTOL, RM Williams, RT Leitner, EO Rogers, DTNSRDC

Flight Testing of the Circulation Control Wing, RJ Englar and AJ Pugliese, AIAA 79-171

The Application of Circulation Control Pneumatic Technology to Powered Lift STOL Aircraft, RJ Englar, SAE 872335, 7/12/87

US Patent 5,601,047 Dual Cavitating Hydrofoil Structures for Multi Speed Applications

US Patent 4,457,480 Mono Element Combined Supercritical High Lift Airfoil to RJ Englar

 
 

Copyright 2005 Meridian International Research
Last updated 22/09/05