Open Access
| Issue |
JNWPU
Volume 37, Number 1, February 2019
|
|
|---|---|---|
| Page(s) | 203 - 210 | |
| DOI | https://doi.org/10.1051/jnwpu/20193710203 | |
| Published online | 03 April 2019 | |
- Donald Howe, Frank Simmons, Don Freund. Development of the Gulfstream Quiet Spike TM for Sonic Boom Minimization[R]. AIAA-2008-0124 [Google Scholar]
- Hua R, Ye Z. Drag Reduction Method for Supersonic Missile Based on Busemann Biplane Concept[J]. Chinese Journal of Applied Mechanics, 2012, 29(5): 535-541 [Article] [Google Scholar]
- Freund D, Howe D, Simmons F, et al. Quiet Spike Prototype Aerodynamic Characteristics from Flight Test[R]. AIAA-2008-0125 [Google Scholar]
- Whitham G. The Flow Pattern of a Supersonic Projectile[J]. Communications on Pure and Applied Mathematics, 1952, 5(3): 289-301 [Article] [CrossRef] [Google Scholar]
- Rallabhandi S K. Advanced Sonic Boom Prediction Using the Augmented Burgers Equation[J]. Journal of Aircraft, 2011, 48(4): 354-360 [Article] [CrossRef] [Google Scholar]
- Park M A, Morgenstern J M. Summary and Statistical Analysis of the First AIAA Sonic Boom Prediction Workshop[J]. Journal of Aircraft, 2015, 98(1): 569-578 [Article] [Google Scholar]
- Farhatt C, Argrow B, Nikbay M, et al. Shape Optimization with F-Function Balancing for Reducing the Sonic Boom Initial Shock Pressure Rise[J]. International Journal of Aeroacoustics, 2004, 3(3): 348-361 [Article] [Google Scholar]
- Li C, Ye Z, Wang G. Simulation of Flow Separation at the Wing-Body Junction with Different Fairings[J]. Journal of Aircraft, 2015, 45(1): 340-358 [Article] [Google Scholar]
- Ma B, Wang G, Ren J, et al. Near Field Sonic Boom Analysis with HUNS3D Solver[R]. AIAA-2017-0038 [Google Scholar]
- Mian H H, Wang G, Raza M A. Application and Validation of HUNS3D Flow Solver for Aerodynamic Drag Prediction Cases[C]//International Bhurban Conference on Applied Sciences and Technology, 2013: 18-20 [Google Scholar]
- Roe P L. Approximate Riemann Soslvers, Parameter Vectors, and Difference Schemes[J]. Journal of Computational Physics, 1981, 43(2): 350-357 [Article] [NASA ADS] [Google Scholar]
- Liou Mengsing. Ten Years in the Making-AUSM-Family[R]. AIAA-2001-2521 [Google Scholar]
- Ismail Farzad, Philip L. Affordable, Entropy-Consistent Euler Flux Functions Ⅱ:Entropy Production at Shocks[J]. Journal of Computational Physics, 2009, 228(15): 365-410 [Article] [Google Scholar]
- Zha G C, Shen Y, Wang B. An Improved Low Diffusion E-CUSP Upwind Scheme[J]. Computers & Fluids, 2011, 48(1): 20-21 [Article] [Google Scholar]
- Jameson A, Schmidt W, Turkel E. Numerical Solution of the Euler Equations by Finite Volume Methods Using Runge Kutta Time Stepping Schemes[R]. AIAA-1981-1259 [Google Scholar]
- Venkatakrishnan V. Convergence to Steady State Solutions of the Euler Equations on Unstructured Grids with Limiters[J]. Journal of Computational Physics, 1995, 118(118): 111-120 [Article] [NASA ADS] [CrossRef] [Google Scholar]
- Spalart P, Allmaras S. A One-Equation Turbulence Model for Aerodynamic Flows[J]. La Recherche Aérospatiale, 1992, 439(1): 5-21 [Article] [Google Scholar]
- Plotkin K J. Review of Sonic Boom theory[R]. AIAA-1989-1105 [Google Scholar]
- Cleveland R O. Propagation of Sonic Booms through a Real, Stratified Atmosphere[D]. Austin, The University of Texas at Austin, 1995 [Google Scholar]
- Howe D. Improved Sonic Boom Minimization with Extendable Nose Spike[R]. AIAA-2005-1014 [Google Scholar]
- Wolz R. A Summary of Recent Supersonic Vehicle Studies at Gulfstream Aerospace[R]. AIAA-2003-0558 [Google Scholar]
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