Active flow control by a novel combinational active thermal protection for hypersonic vehicles
Effect of spike on steady and unsteady flow over a blunt body at supersonic speed
Aerothermodynamics of blunt body entry vehicles
Reduction of wave drag on parameterized blunt bodies using spikes with varied tip geometries
Aero-spike and aero-disk effects of on wave drag reduction of supersonic flow past over blunt body
Design and Technology Maturation of the Stratospheric Projectile Experiment of Entry Dynamics
An analytical approach for stand-off distance of detached shock waves
Experimental analysis of shock stand-off distance over spherical bodies in high-enthalpy flows
Interaction between laser-induced plasma and shock wave over a blunt body in a supersonic flow
Free-flight tests of a blunt-nosed flare- stabilized body at speeds to 8.2 km/sec.
Heating of an Anisotropic Insulation Layer with Hypersonic Flow Past a Spherical Blunting
Heating of an Anisotropic Insulation Layer with Hypersonic Flow Past a Spherical Blunting
Free-flight tests of a blunt-nosed flare- stabilized body at speeds to 8.2 km/sec.
Longitudinal stability characteristics of several proposed planetary entry vehicles at mach 6.73
Pressure distribution on forward face of blunt bodies at angle of attack.
SHOCK-LAYER RADIATION OF BLUNT BODIES TRAVELING AT LUNAR RETURN ENTRY VELOCITIES
Viscous Damping of Roll During Entry of a MARS Entry and Landing Capsule
Epidemiologic Study on Work‐related Eye Injuries in Kaohsiung, Taiwan
Free-flight aerodynamics of a blunt-faced reentry shape with and without ablation.
Three-dimensional flow calculation by the method of characteristics.
Quantitative Assessment of Aerocapture and Applications to Future Solar System Exploration
Symmetrical, equilibrium flow past a blunt body at superorbital re-entry speeds.
Feasibility and Mass-Benefit Analysis of Aerocapture for Missions to Venus
Hypersonic flow over a blunt flat plate with surface mass transfer.
Force Measurements on Blunt Bodies in the Dvl- Gun Tunnel ( M 8 to 16)
Effect of forward-facing jets on aerodynamic characteristics of blunt configurations at Mach 6.