N. S. Dougherty

发表

Space Shuttle Propulsion Systems Plume Modeling and Simulation for the Lift-Off Computational Fluid Dynamics Model

Louise L. Strutzenberg, N. S. Dougherty, Peter A. Liever, 2007 .

Liquid Rocket Engine Testing - Historical Lecture: Simulated Altitude Testing at AEDC

N. S. Dougherty, 2010 .

Four-Nozzle Benchmark Wind Tunnel Model USA Code Solutions for Simulation of Multiple Rocket Base Flow Recirculation at 145,000 Feet Altitude

N. S. Dougherty, S. L. Johnson, 1993 .

Computational fluid dynamics analysis of Space Shuttle main engine multiple plume flows at high-altitude flight conditions

J. B. Holt, N. S. Dougherty, B. L. Liu, 1992 .

Computational fluid dynamics analysis of Space Shuttle vehicle and exhaust plume flows at high-altitude flight conditions

N. S. Dougherty, Spencer Johnson, Johnson Holt, 1992 .

Boundary-Layer Transition Correlation on a Slender Cone in Wind Tunnels and Flight for Indications of Flow Quality

N. S. Dougherty, D. Fisher, N. Dougherty, 1982 .

A correlation of scale model and flight aeroacoustic data for the Space Shuttle vehicle

S. H. Guest, N. S. Dougherty, 1984 .

Boundary-layer transition on a 10-deg cone - Wind tunnel/flight correlation

N. S. Dougherty, D. F. Fisher, 1980 .

Transition Reynolds number comparisons in several major transonic tunnels

N. S. Dougherty, F. W. Steinle, 1974 .

Flight and wind-tunnel correlation of boundary-layer transition on the AEDC transition cone

N. S. Dougherty, D. F. Fisher, 1982 .