Effects of reaction control system jet simulation on the stability and control characteristics of a 0.015-scale space shuttle orbiter model in the Ames Research Center 3.5-foot hypersonic wind tunnel [PDF]
An experimental investigation was performed in the Ames Research Center 3.5-Foot Hypersonic Wind Tunnel to obtain detailed effects which interactions between the RCS jet flow field and the local orbiter flow field have on orbiter hypersonic stability and
Cleary, J. W. +3 more
core +1 more source
Magnetohydrodynamic simulations of hypersonic flow over a cylinder using axial- and transverse-oriented magnetic dipoles. [PDF]
Guarendi AN, Chandy AJ.
europepmc +1 more source
Internal convective cooling systems for hypersonic aircraft [PDF]
Parametric studies were conducted to investigate the relative merits of construction materials, coolants, and cooled panel concepts for internal convective cooling systems applied to airframe structures of hydrogen-fueled hypersonic aircraft.
Anthony, F. M. +2 more
core +1 more source
Experimental study of fluid-thermal-structural interactions in a Mach-10 compression corner using super-ellipse-based photogrammetry. [PDF]
Duchene TA +6 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
Hypersonic turbulent quantities in support of Morkovin's hypothesis. [PDF]
Segall BA +6 more
europepmc +1 more source
Mitigating hypersonic heat barrier via direct cooling enhanced by leidenfrost inhibition. [PDF]
Wang JX +6 more
europepmc +1 more source
Influence of Flow Field on the Imaging Quality of Star Sensors for Hypersonic Vehicles in near Space. [PDF]
Wu S +7 more
europepmc +1 more source
High-Reynolds-Number Turbulence Database: AeroFlowData. [PDF]
Zhang W +18 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

