Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight
By: W. Derry Mace ... [et al.].
Contributors: Mace, W. Derry.; Langley Research Center.
Series: [NASA technical memorandum] -- 109040, v. 1-<4>; NASA technical memorandum -- 109040.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1993
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Laser Doppler velocimeter.; Rotors (Helicopters) -- Aerodynamics.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0429-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994-    ] microfiche .
Table of contents: value: v. 1. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 603 ft/sec; value: v. 2. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 710 ft/sec; value: v. 3. Laser velocimeter inflow data, advance ratio of 0.37, thrust coefficient of 0.0064 and hover tip speed of 603 ft/sec; value: v. 4. Laser velocimeter wake data, advance ratio of 0.37.