Results 61 to 70 of about 8,682,927 (148)
Shock Angle Characteristics and Test Analysis of Hypersonic Wide-Speed-Range Cruise Aircraft
AerospaceHypersonic aircraft represent a cutting-edge technology in aerospace engineering, where the shock angle serves as a critical aerodynamic parameter. However, existing studies remain limited by significant prediction errors for the shock angle.
Shuailong Gao +3 more
doaj +1 more source
Bifurcating Mach Shock Reflections with Application to Detonation Structure
, 2011 Numerical simulations of Mach shock reflections have shown that the Mach stem can bifurcate as a result of the slip line jetting forward. Numerical simulations were conducted in this study which determined that these bifurcations occur when the Mach ...
Mach, Philip
core +2 more sources
Interpreting Ernst Mach: Critical Essays
, 2021 Erik Banks, to whom this volume is dedicated, was at the forefront of the major recent re-evaluation of the works of physicist, psychologist and philosopher Ernst Mach. This volume presents the latest in-depth research on Mach’s work and thought.
core +1 more source
Numerical study of high speed separated flows
, 2014 Instability, flow separation and transition are essential aspects of high speed flows with shock-wave/boundary-layer interaction. Supersonic flows with jet injection, compression ramp and cavity, either individually or in combination, are numerically ...
Zhang, Kangping
core +1 more source
Hypersonic interference heating in the vicinity of surface protuberances [PDF]
, 2010 The understanding of the behaviour of the flow around surface protuberances in hypersonic vehicles is developed and an engineering approach to predict the location and magnitude of the highest heat transfer rates in their vicinity is presented.
Garry, Kevin P. +4 more
core +1 more source
, 2012 Above a certain Mach number, several aerodynamic properties become asymptotically independent of the free stream Mach number, such as pressure coefficient, lift and wave-drag coefficients, and flow-field structure.
Li JP(李进平) +2 more
core +2 more sources
Numerical Analysis of Supersonic Film Cooling in Supersonic Flow in Hypersonic Inlet with Isolator
Advances in Mechanical Engineering, 2014 Supersonic film cooling is an efficient method to cool the engine with extremely high heat load. In order to study supersonic film cooling in a real advanced engine, a two-dimensional model of the hypersonic inlet in a scramjet engine with supersonic ...
Silong Zhang +3 more
doaj +1 more source
A Study of the Complex Flow Features Behind a Diffracted Shock Wave on a Convex Curved Wall
Journal of Applied Fluid Mechanics, 2015 The complex flow features behind a diffracted shock wave on a convex curved wall is investigated using large scale experimentation complemented by numerical computation.
adam muritala, B. Skews, craig law
doaj
Research on Refined Design Method for Large-Diameter Hypersonic Nozzle Contours
AerospaceWith the advancement of aerospace technology, full-scale wind tunnel testing has become a crucial approach to overcoming bottlenecks in hypersonic technology.
Chenxi Sun +3 more
doaj +1 more source
Shock Mach Number Estimates Using Incomplete Measurements
, 2021 The Mach number is one of the most important parameters of collisionless shocks. The accuracy of its observational determination is compromised by several complications.
Dimmock, Andrew P., +8 more
core +1 more source