The well-posedness issue for an inviscid zero-Mach number system in general Besov spaces
, 2015 Francesco Fanelli, Xian Liao
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A CRITICAL SHOCK MACH NUMBER FOR PARTICLE ACCELERATION IN THE ABSENCE OF PRE-EXISTING COSMIC RAYS: $M=\sqrt{5}$ [PDF]
, 2013 Jacco Vink, Ryo Yamazaki
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Ground Measurements of Airplane Shock-Wave Noise at Mach Numbers to 2.0 and at Altitudes to 60,000 Feet [PDF]
The intensity of shock-wave noise at the ground resulting from flights at Mach numbers to 2.0 and altitudes to 60,000 feet was measured. Meagurements near the ground track for flights of a supersonic fighter and one flight of a supersonic bomber are ...
Lina, Lindsay J., Maglieri, Domenic J.
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Splitting methods for low Mach number Euler and Navier-Stokes equations [PDF]
Examined are some splitting techniques for low Mach number Euler flows. Shortcomings of some of the proposed methods are pointed out and an explanation for their inadequacy suggested.
Abarbanel, Saul +2 more
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The impact of inlet mach number and domain shape on subsonic nozzle flow via small disturbance equation [PDF]
, 2023 Xuehui Qian
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SLAMS-propelled Electron Acceleration at High-Mach-number Astrophysical Shocks
The Astrophysical JournalShort large-amplitude magnetic structures (SLAMS) are frequently detected during spacecraft crossings over Earth's bow shock. We investigate the existence of such structures at astrophysical shocks, where they could result from the steepening of cosmic ...
Vladimir Zeković +2 more
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Revisiting the structure of low-Mach number, low-beta, quasi-perpendicular shocks. [PDF]
J Geophys Res Space Phys, 2017 Wilson LB +6 more
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Fully Compressible Low-Mach Number Simulations of Carbon-dioxide at Supercritical Pressures and Trans-critical Temperatures. [PDF]
Flow Turbul Combust, 2017 Sengupta U +3 more
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Application of numerical optimization to the design of advanced supercritical airfoils [PDF]
An application of numerical optimization to the design of advanced airfoils for transonic aircraft showed that low-drag sections can be developed for a given design Mach number without an accompanying drag increase at lower Mach numbers. This is achieved
Hicks, R. M., Johnson, R. R.
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