From the fall of 1993 to late winter of 1994, NASA Ames and the U.S. Army flew a flight test program using a UH-60A helicopter with extensive instrumentation on the rotor and blades, including 242 pressure transducers. Over this period, approximately 30 flights were made, and data were obtained in level flight, maneuver, ascents, and descents. Coordinated acoustic measurements were obtained with a ground-acoustic array in cooperation with NASA Langley, and in-flight acoustic measurements with a YO-3A aircraft. NASA has sponsored the creation of a "tutorial' which covers the depth and breadth of the flight test program with a mixture of text and graphics. The primary purpose of this tutorial is to introduce the student to what is known about rotor aerodynamics based on the UH-60A measurements. The tutorial will also be useful to anyone interested in helicopters who would like to have more detailed knowledge about helicopter aerodynamics.
UH-60 Airloads Program Tutorial
AHS 65th Annual Forum and Technology Display ; 2009 ; Grapevine, TX
2009-05-27
Conference paper
No indication
English
USAAVLABS tandem rotor airloads measurement program.
AIAA | 1967
|USAAVLABS tandem rotor airloads measurement program
Engineering Index Backfile | 1967
|UH-60 Airloads Program - Status and plans
AIAA | 1991
|UH-60 Airloads Program - Status and plans
NTRS | 1991
|The USAAVLABS tandem rotor airloads measurement program
AIAA | 1966
|