Using temperature sensitive paint technology

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Hamner, M P ^a   Popernack Jr , T G ^b   Owens, L R ^b   Wahls, R A ^b  

^a LeaTech   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 78549241023     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Kuethe. A.M. and Chow, C.Y. (1986) Foundations of Aerodynamics, Bases of Aerodynamic Design: Fourth Edition, Wiley: New York.
2. Morkovin. M.V. (1988) Recent Insights into Instability and Transition to Turbulence in Open-Flow Systems, AIAA Paper 88-3675.
3. Popernack, Jr., T.G., Owens, L.R., Hamner, M.P. and Morris, MJ. (1997) Application of Temperature Sensitive Paint for Detection of Boundary Layer Transition. ICIASF.
4. Schlichting, H. (1979) Boundary-Layer Theory, McGraw-Hill. Inc.: New York.
5. Incropera, P.P. and DeWitt, D.P. (1981) Fundamentals of Heat and Mass Transfer, John Wiley & Sons: New York
6. Campbell, B.T. (1993) Temperature Sensitive Fluorescent Paints for Aerodynamic Applications. M.S. Thesis, School of Aeronautics and Astronautics, Purdue University, West Lafayette, IN.
7. Clutter, D.W. (1959) Charts for Determining Skin-Friction Coefficients on Smooth and Rough Flat Plates at Mach Numbers up to 5.0 with and without Heat Transfer, ES 29074.
8. Braslow, A.L., Hicks, R.M. and Harris, Jr., R.V. (1966) Use of Grit-Type Boundary-Layer Transition Trips on Wind-Tunnel Models, NASA TN D-3579.
9. Hefner, J.N. and Sabo, F.E. (1987) Research in Natural Laminar flow and Laminar-Flow Control, NASA CP-2487 Part 3.
10. Johnson, W.G., Jr., Hill, A.S. and Eichmann, O. (1985) High Reynolds Number Tests of a NASA SCO)-0712(B) Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel, NASA TM-86371.
11. Hamner, M.P., Kelble, C.A., Owens, L.R. and Popernack, Jr., T.G. (1997) Application of Temperature Sensitive Paint Technology to Boundary Layer Analysis, AIAA Paper No. 97-5536.
12. Liepmann, H.W. and Roshko. A. (1957) Elements of Gas Dynamics, Wiley: New York.