An edge-based solution-adaptive method applied to the AIRPLANE code | Libros

High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

Robert S. Jankovsky

1999

2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall

R. A. Piziali

1994

Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code

Wendy B. Lessard

1996

F-18 High Alpha Research Vehicle surface pressures

David F. Fisher

1990

Laser scanning system for pressure and temperature paints

John Sullivan

1997

Analysis of two-phase flow in damper seals for cryogenic turbomachinery

Grigory L. Arauz

1996

Enhanced design of turbo-jet LPT by separation control using phased plasma actuators

Thomas C. Corke

2003

Rocket-based combined cycle engine technology development

J. R. DeBonis

1996