Airloads Research Study. Volume 1: Flight Test Loads Acquisition
Airloads Research Study. Volume 1: Flight Test Loads Acquisition
- New search for: M. D. Bartlett
- New search for: T. F. Feltz
- New search for: A. D. Olsen
- New search for: D. B. Smith
- New search for: P. F. Wildermuth
- New search for: M. D. Bartlett
- New search for: T. F. Feltz
- New search for: A. D. Olsen
- New search for: D. B. Smith
- New search for: P. F. Wildermuth
The acquisition of B-1 aircraft flight loads data for use in subsequent tasks of the Airloads Research Study is described. The basic intent is to utilize data acquired during B-1 aircraft tests, analyze these data beyond the scope of Air Force requirements, and prepare research reports that will add to the technology base for future large flexible aircraft. Flight test data obtained during the airloads survey program included condition-describing parameters, surface pressures, strain gage outputs, and loads derived from pressure and strain gauges. Descriptions of the instrumentation, data processing, and flight load survey program are included. Data from windup-turn and steady yaw maneuvers cover a Mach number range from 0.7 to 2.0 for a wing sweep position of 67.5 deg.
Document information
Airloads Research Study. Volume 1: Flight Test Loads Acquisition
1984
134 pages
Report
No indication
English
Similar titles
Investigation of Rotor Airloads and Structural Loads in Maneuvering Flight
| British Library Conference Proceedings | 2008
UH-60A Airloads Flight Test Program: Data Counter 8534
| NTRS | 2019
UH-60A Airloads Flight Test Program: Data Counter 9505
| NTRS | 2019
UH-60A Airloads Flight Test Program: Data Counter 8513
| NTRS | 2019