Effect of Scarfing on Rectangular Nozzle Supersonic Jet Plume Flow Characteristics
Author:
Affiliation:
1. Loughborough University, Loughborough, England LE11 3TU, United Kingdom
2. Rolls–Royce, plc, Bristol, England BS34 7QE, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055526
Reference31 articles.
1. Nonaxisymmetric Nozzles Installed in Advanced Fighter Aircraft
2. ShyneR. J. “A Survey of Challenges in Aerodynamic Exhaust Nozzle Technology for Aerospace Propulsion Applications,” NASA TM-2002-211977, Nov. 2002.
3. Nozzle Selection and Design Criteria
4. LambM.TaylorJ. G.FrassinelliM. C. “Static Internal Performance of a 2-D Con-Di Nozzle with External Shelf,” NASA TM 4719, Sept. 1996.
5. Infrared signature studies of aerospace vehicles
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