The problem of shock wave/boundary layer interaction induced by compression corners widely exists in the external and internal flows of various supersonic/hypersonic aircraft.
Dongsheng Zhang +3 more
doaj +1 more source
Investigation of Stability and Control Shortcomings of the North American X-15
There is growing interest in the design of maneuvering high-speed aircraft to fly within or at the edge of the atmosphere. We identify and develop novel quasi-static vehicle screening methodologies, suitable for use during preliminary design, to better ...
William P. Lorenzo +2 more
doaj +1 more source
Quasiclassical trajectory computations of elementary processes in air hypersonic flows
Collision processes of heavy particles: Quasiclassical trajectory computations of elementary processes in air hypersonic ...
Esposito, Fabrizio
core
State-to-state approach in hypersonic thermochemical nonequilibrium flow simulations: a review. [PDF]
Chu X +6 more
europepmc +1 more source
Multilevel Physiological Responses to the Hypersonic Effect: Concurrent Electroencephalographic, Heart Rate Variability, and Subjective Evaluation in Healthy Adults in a Participant-Blind Crossover Study. [PDF]
Takasao G +7 more
europepmc +1 more source
Research on Star Sensor Imaging Simulation Under Near-Space Hypersonic Non-Equilibrium Flow Conditions. [PDF]
Liao Z +7 more
europepmc +1 more source
Hypersonic levitation and spinning: paving the way for enhanced single-cell analysis via contactless tissue dissociation. [PDF]
Bai Y +5 more
europepmc +1 more source
Experimental study of nose-tip bluntness effects on hypersonic boundary-layer transition in a shock tunnel. [PDF]
Kim J, Nam J, Hur J, Kim J, Lee BJ.
europepmc +1 more source
Collision Integrals for Transport in Plasmas: The Phenomenological Approach. [PDF]
Pirani F +3 more
europepmc +1 more source
Hypersonic turbulent quantities in support of Morkovin's hypothesis. [PDF]
Segall BA +6 more
europepmc +1 more source

