Experimental investigation of separated nozzle flows

Journal of Propulsion and Power

Volumn 20, Issue 3, 2004, Pages 527-532

  Hunter, Craig A ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Distinguished Research Associate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; BOUNDARY LAYERS; FLOW VISUALIZATION; GAS DYNAMICS; MATHEMATICAL MODELS; NOISE ABATEMENT; RESEARCH LABORATORIES; SUPERSONIC FLOW; VISCOUS FLOW;

MACH NUMBER; NOISE SUPPRESSION; NOZZLE AREA; NOZZLE PRESSURE RATIO (NPR);

NOZZLES;

EID: 2942565888     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.4612     Document Type: Article

References (13)

1. Lewis, W. G. E., "Propelling Nozzle Research," Journal of the Royal Aeronautical Society, Vol. 68, Nov. 1964, pp. 717-727.
2. Asbury, S. C., Gunther, C. L., and Hunter, C. A., "A Passive Cavity Concept for Improving the Off-Design Performance of Fixed-Geometry Exhaust Nozzles," AIAA Paper 96-2541, July 1996.
3. Hunter, C. A., "An Experimental Analysis of Passive Shock-Boundary Layer Interaction Control for Improving the Off-Design Performance of Jet Exhaust Nozzles," M.S. Thesis, Joint Institute for Advancement of Right Sciences, George Washington Univ., Washington, DC, Sept. 1993.
4. Propulsion Aerodynamics Branch Staff, "A User's Guide to the Langley 16-Foot Transonic Tunnel Complex, Revision 1," NASA TM-102750, Sept. 1990.
5. Capone, F. J., Bangert, L. S., Asbury, S. C., Mills, C. T., and Bare, E. A., "The NASA Langley 16-Foot Transonic Tunnel: Historical Overview, Facility Description, Calibration, Flow Characteristics, and Test Capabilities," NASA TP-3521, Sept. 1995.
6. Mercer, C. E., Berrier, B. L., Capone, F. J., and Grayston, A. M., "Data Reduction Formulas for the 16-Foot Transonic Tunnel at NASA Langley Research Center, Revision 2," NASA TM-107646, July 1992.
7. Coleman, H. W., and Steele, W. G., Jr., Experimentation and Uncertainty Analysis for Engineers, Wiley, New York, 1989, Chap. 1-7.
8. Wing, D. J., Mills, C. T. L., and Mason, M. L., "Static Investigation of a Multiaxis Thrust-Vectoring Nozzle With Variable Internal Contouring Ability," NASA TP-3628, June 1997.
9. Weinstein, L. M., "An Improved Large-Field Focusing Schlieren System," AIAA Paper 91-0567, Jan. 1991.
10. Hunter, C. A., "An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-Dimensional Convergent-Divergent Nozzles," NASA CR-195050, March 1995.
11. Anderson, J. D., Modern Compressible Flow with Historical Perspective, McGraw-Hill, New York, 1982, Chap. 5.
12. Capone, F. J., Konarski, M., Stevens, H. L., and Willard, C. M., "Static Performance of Vectoring/Reversing Non-axisymmetric Nozzles," AIAA Paper 77-840, July 1977.
13. Leavitt, L. D., "Summary of Nonaxisymmetric Nozzle Internal Performance from the NASA Langley Static Test Facility," AIAA Paper 85-1347, July 1985.