B. W. Sanders

Aerodynamic Design of a Dual-Flow Mach 7 Hypersonic Inlet System for a Turbine-Based Combined-Cycle Hypersonic Propulsion System

B. W. Sanders, Lois J. Weir · NASA Technical Reports Server (NASA) · 2008 · 47 citations · Full text

Engineering, Aerodynamic Design, Mechanical Engineering +17

Highlights from a Mach 4 Experimental Demonstration of Inlet Mode Transition for Turbine-Based Combined Cycle Hypersonic Propulsion

Lancert Foster, John Saunders, B. W. Sanders et al. · 2012 · 29 citations · Full text

Mach 4, Engineering, Inlet Mode Transition +16

Effect of bleed-system back pressure and porous area on the performance of an axisymmetric mixed-compression inlet at Mach 2.50

R. W. Cubbison, B. W. Sanders · NASA Technical Reports Server (NASA) · 1968 · 21 citations

Unsteady Flow, Compressible Flow, Engineering +13

Testing of the NASA Hypersonics Project Combined Cycle Engine Large Scale Inlet Mode Transition Experiment (CCE LlMX)

John Saunders, Thomas J. Stueber, Scott Thomas et al. · NASA Technical Reports Server (NASA) · 2012 · 18 citations

Aeroacoustics, Engineering, Hypersonic Propulsion +16

Role of CFD in the Aerodynamic Design and Analysis of the Parametric Inlet

John W. Slater, David O. Davis, B. W. Sanders et al. · 2005 · 16 citations

Unsteady Flow, Engineering, Aerospace Engineering +6