Add to ORKGIn a continuing effort to understand helicopter rotor tip aerodynamics and acoustics, a flight test was conducted by NASA Ames Research Center. The test was performed using the NASA White Cobra and a set of highly instrumented blades. All aspects of the flight test instrumentation and test procedures are explained. Additionally, complete data sets for selected test points are presented and analyzed. Because of the high volume of data acquired, only selected data points are presented. However, access to the entire data set is available to the researcher on request
A flight test program was performed using the Boeing 757 flight research airplane to investigate the...
The separated flow method is evaluated. This method was developed for moderately swept wings with mu...
Efforts were focused on design problems of an unmanned hypersonic vehicle. It is felt that a scaled ...
Wake vortices from a C-130 airplane were observed at the NASA Wallops Flight Facility with a ground-...
A number of facilities were developed which provide unique test capabilities for aeroacoustic resear...
This report is section VIII of a series of reports on aeronautic instruments. The preceding reports ...
The sonic boom propagation codes reviewed in this study, SHOCKN and ZEPHYRUS, implement current theo...
A piloted simulator experiment was conducted to investigate directional axis handling qualities requ...
A technique was developed which provides reliable failure detection and identification (FDI) for a d...
A modular computer program (ANOPP) for predicting aircraft flyover and sideline noise was developed....
Ultrahigh frequency air traffic control satellite simulation experiment using high altitude balloon
The various activities and findings of a NASA/FAA/COMSAT/INMARSAT collaborative aeronautical mobile ...
Herein is presented the collected data for tests in which a NACA 23012A aerofoil was subjected to a ...
Work performed by the McDonnell Douglas Helicopter Company and Lucas Western, Inc. within the U.S. A...
Primarily an experimental effort, this study focuses on the velocity and vorticity fields in the nea...
A flight test program was performed using the Boeing 757 flight research airplane to investigate the...
The separated flow method is evaluated. This method was developed for moderately swept wings with mu...
Efforts were focused on design problems of an unmanned hypersonic vehicle. It is felt that a scaled ...
Wake vortices from a C-130 airplane were observed at the NASA Wallops Flight Facility with a ground-...
A number of facilities were developed which provide unique test capabilities for aeroacoustic resear...
This report is section VIII of a series of reports on aeronautic instruments. The preceding reports ...
The sonic boom propagation codes reviewed in this study, SHOCKN and ZEPHYRUS, implement current theo...
A piloted simulator experiment was conducted to investigate directional axis handling qualities requ...
A technique was developed which provides reliable failure detection and identification (FDI) for a d...
A modular computer program (ANOPP) for predicting aircraft flyover and sideline noise was developed....
Ultrahigh frequency air traffic control satellite simulation experiment using high altitude balloon
The various activities and findings of a NASA/FAA/COMSAT/INMARSAT collaborative aeronautical mobile ...
Herein is presented the collected data for tests in which a NACA 23012A aerofoil was subjected to a ...
Work performed by the McDonnell Douglas Helicopter Company and Lucas Western, Inc. within the U.S. A...
Primarily an experimental effort, this study focuses on the velocity and vorticity fields in the nea...
A flight test program was performed using the Boeing 757 flight research airplane to investigate the...
The separated flow method is evaluated. This method was developed for moderately swept wings with mu...
Efforts were focused on design problems of an unmanned hypersonic vehicle. It is felt that a scaled ...
