Pressure sensitive paint demonstrates relationship between ejector wall pressure and aerodynamic performance

Experiments in Fluids

Volumn 26, Issue 6, 1999, Pages 481-487

  Taghavi, R ^a   Raman, G ^b   Bencic, T ^b  

^a University of Kansas   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

JETS; NOZZLES; PAINT; PRESSURE DISTRIBUTION; SUPERSONIC AERODYNAMICS; WALL FLOW;

MIXER-EJECTOR NOZZLES; PRESSURE SENSITIVE PAINTS (PSP);

SUPERSONIC FLOW;

EID: 0032685785     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s003480050314     Document Type: Article

References (9)

1. Bell JN; McLachlan BG (1996) Image registration for pressure-sensitive paint applications. Exp Fluids 22: 78-86
2. Bencic TJ (1995) Experiences using pressure sensitive paint in NASA. Lewis Research Center Propulsion Test Facilities. AIAA Paper 95-2831
3. Cler D; Lamb M; Farokhi S; Taghavi R; Hazlewood R (1996) Application of pressure-sensitive paint in supersonic nozzle research. J Aircraft 33:1109-1114
4. McLachlan BG; Kavandi J; Gouterman M; Green D; Khalil G; Burns D (1992) Surface pressure field mapping using luminescent coatings. Exp Fluids 14: 33-41
5. Morris MJ; Donovan JF (1994) Application of pressure and temperature sensitive paint to high speed flows. AIAA Paper 94-2231
6. Raman G; Taghavi R (1997) Aeroacoustics characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle. J Sound Vib 207: 227-248
7. Rice EJ (1995) Jet mixer noise suppressor using acoustic feedback. US Patents 5,325,661, and 5,392,597
8. Taghavi R; Raman G (1996) Flow characteristics of a rectangular multi-element supersonic mixer-ejector. J Propulsion and Power 12: 1004-1107
9. Taghavi R; Raman G; Bencic T (1998) Mixer-ejector wall pressure and temperature measurements based on photoluminescence. ASME FEDSM 98-5085