Effect of Mass Flow Rate on Drag Reduction with Counter-Flow Jet in Laminar Hypersonic Flow at High Reynolds Number
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-3998-1_130
Reference17 articles.
1. Bogdonoff, S.M., Vas, F.: Preliminary investigations of spiked bodies at hypersonic speeds. J. Aerospace Sci. 26, 65–74 (1959)
2. Feszty, D., Badcock, K.J., Richards, B.E.: Driving mechanism of high-speed unsteady spiked body flows, part i: pulsation mode. AIAA J. 42, 95–106 (2004)
3. Panaras, A.G., Drikakis, D.: High-speed unsteady flows around spiked-blunt bodies. J. Fluid Mech. 632, 69–96 (2009)
4. Osuka, T., et al.: Laser energy deposition effectiveness on shock-wave boundary-layer interactions over cylinder-flare combinations. Phys. Fluids 26, 096103 (2014)
5. Huebner, L., Mitchell, A., Boudreaux, E.: Experimental results on the feasibility of an aero-spike for hypersonic missiles. In: 33rd Aerospace Sciences Meeting and Exhibit (1995). https://arc.aiaa.org/doi/pdf/10.2514/6
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