UH-60 Airloads Program TutorialFrom 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.
Document ID
20090036797
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Bousman, William G. (Monterey Technologies, Inc. United States)
Date Acquired
August 24, 2013
Publication Date
May 27, 2009
Subject Category
Aerodynamics
Report/Patent Number
ARC-E-DAA-TN517Report Number: ARC-E-DAA-TN517
Meeting Information
Meeting: AHS 65th Annual Forum and Technology Display