David M. Richwine

发表

Flight-Test Fixture For Aerodynamic Research

David M. Richwine, John H. Del Frate, 1995 .

Advanced Video Data-Acquisition System For Flight Research

Neal E. Hass, David M. Richwine, Geoffrey Miller, 1996 .

An airborne system for vortex flow visualization on the F-18 high-alpha research vehicle

R. E. Curry, Robert E. Curry, David M. Richwine, 1988 .

Development of a low-aspect ratio fin for flight research experiments

David M. Richwine, John H. Delfrate, 1994 .

Surface flow visualization of separated flows on the forebody of an F-18 aircraft and wind-tunnel model

Daniel W. Banks, David M. Richwine, David F. Fisher, 1988 .

F-15B/Flight Test Fixture 2: A Test Bed for Flight Research

David M. Richwine, 1996 .

A smoke generator system for aerodynamic flight research

R. E. Curry, Robert E. Curry, David M. Richwine, 1989 .

Smoke Generator For Studies Of Vortices In Flight

Robert E. Curry, David M. Richwine, Gene V. Tracy, 1992 .

A TEST BED FOR FLIGHT RESEARCH EXPERIMENTS

David M. Richwine, 1997 .

Correlation of forebody pressures and aircraft yawing moments on the X-29A aircraft at high angles of attack

David M. Richwine, David F. Fisher, D. Fisher, 1992 .

In-Flight Flow Visualization Characteristics of the NASA F-18 High Alpha Research Vehicle at High Angles of Attack

David M. Richwine, John H. Del Frate, David F. Fisher, 1989 .

F-18 high alpha research vehicle surface pressures: Initial in-flight results and correlation with flow visualization and wind-tunnel data

Daniel W. Banks, David M. Richwine, David F. Fisher, 1990 .

In-flight leading-edge extension vortex flow-field survey measurements on a F-18 aircraft at high angle of attack

David M. Richwine, David F. Fisher, D. Fisher, 1991 .