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Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight [microform] / W. Derry Mace [and others]

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Bibliographic Details
Corporate Author:	Langley Research Center
Other Authors:	Mace, W. Derry
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1993-]
Series:	NASA technical memorandum ; 109040.
Subjects:	Laser Doppler velocimeter. Rotors (Helicopters) > Aerodynamics.

Table of Contents:

v. 1. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 603 ft/sec
v. 2. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 710 ft/sec
v. 3. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 603 ft/sec
v. 4. Laser velocimeter wake data, advance ratio of 0.37.