An Innovative flow-measuring device: Thermocouple boundary layer rake

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Hwang, Danny P ^a   Fralick, Gustave C ^a   Martin, Lisa C ^a   Wrbanek, John D ^a   Blaha, Charles A ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b Akima Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; FLOW MEASUREMENT; THERMOCOUPLES;

FLOW BYES; MEASURING DEVICE; TEMPERATURE DIFFERENCES; THIN FILM THERMOCOUPLE; TOTAL PRESSURE; VELOCITY PROFILES;

BOUNDARY LAYERS;

EID: 85087190196     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-289     Document Type: Conference Paper

References (8)

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2. Bui, Trong T.; Gates, David L.; and Gonsalez, Jose C.: Design and Evaluation of a New Boundary-Layer Rake for Flight Testing. AIAA 2000-0503,2000.
3. Ligrani, P.M.; and Bradshaw, P.: Subminiature Hot-Wire Sensors: Development and Use. J. Phys. E: Sci. Instrum., vol. 20, 1987, pp. 323-332.
4. Ligrani, P.M.; and Bradshaw, P.: Spatial Resolution and Measurement of Turbulence in the Viscous Sublayer Using Subminiature Hot-Wire Probes. Exp. Fluids, vol. 5, no. 6, 1987, pp. 407-417.
5. Doiron, M.D.; and Zingg, D.W.: Turbulent Flow Measurements With a Triple-Split Hot-Film Probe. AIAA J., vol. 32, no. 9, 1994, pp. 1929-1931.
6. Kinzie, P.A.: Thermocouple Temperature Measurement. John Wiley & Sons, New York, NY, 1973.
7. Hwang, Danny P.: A Proof of Concept Experiment for Reducing Skin Friction by Using a Micro-Blowing Technique. AIAA Paper 97-0546, 1997.
8. Schlichting, Hermann: Boundary Layer Theory. Fourth ed., McGraw-Hill, New York, NY, 1960.