241 



Tullahoma, TN., U.S.A. 



16-FOOT SUPERSONIC PROPULSION WIND TUNNEL 

 Arnold Engineering Development Center 

 U.S. Air Force 



"Big Science" Descriptor ; Aerodynamics 



Description of Facility/ Instrument ; This tunnel Is used for both 

 aerodynamic and propulsion system testing. 



Date of Construction ; 1954 



Construction Cost ; 1984 $$ ; $550 million 



Present International Cooperation 



Natlonality(s) of Ownership ; U.S. 

 Natlonallty(s) of Operational Funding ; U.S. 

 Natlonality(s) of Management Staff ; U.S. 

 Natlonallty(s) of Researchers; U.S. 



Tullahoma, TN., U.S.A. 



16-FOOT TRANSONIC PROPULSION WIND TUNNEL 

 Arnold Engineering Development Center 

 U.S. Air Force 



"Big Science" Descriptor ; Aerodynamics 



Description of Facility/Instrument ; This facility conducts force and 

 moment pressure, dynamic stability, jet effects, decelerator de- 

 ployment, internal duct flow, and flutter buffet tests. 



Date of Construction ; 1952 



Construction Cost ; 1984 $$ : $300 million 



Present International Cooperation 



Nationallty(s) of Ownership : U.S. 

 Natlonallty(s) of Operational Funding ; U.S. 

 Natlonality(s) of Management Staff ; U.S. 

 Natlonallty(s) of Researchers; U.S. 



