Effect of Pressure Ratio on Aerodynamic Heating Reduction due to Opposing Jet

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	Year	Citations
Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds LESTER LEES Jet propulsion AerothermodynamicsRadiative Heat TransferHeat Transfer ProcessEngineeringAerospace Engineering	1956	888
The flow of a jet from a body opposing a supersonic free stream Priscilla Finley Journal of Fluid Mechanics AeroacousticsUnsteady FlowEngineeringAerospace EngineeringSteady Flow	1966	284
An experimental investigation of the effect of ejecting a coolant gas at the nose of a bluff body C. H. E. Warren Journal of Fluid Mechanics	1960	152
Thermal protection and drag reduction with use of spike in hypersonic flow Noboru Motoyama, Ken Mihara, Ryo Miyajima, 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference EngineeringThermal ProtectionAerospace EngineeringFluid MechanicsAerodynamics	2001	94
Axisymmetric oscillations of an opposing jet from a hemispherical nose Masahiro Fujita AIAA Journal Flow ControlEngineeringFluid MechanicsSonic Opposing JetTurbulence	1995	39
Rotating Motion Control of Tethered Satellite Cluster Systems. Osamu Mori, Saburo Matunaga JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES Motion ControlCoordinated MissionEngineeringTether TensionAerospace Engineering	2002	10

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