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:

MARC

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245 0 0 |a Investigation of the aerodynamic environment for an advanced lightweight rotor in forward flight  |h [microform] /  |c W. Derry Mace [and others] 
260 |a Hampton, Va. :  |b National Aeronautics and Space Administration, Langley Research Center ;  |a [Springfield, Va.] :  |b [National Technical Information Service, distributor],  |c [1993-] 
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505 1 |a 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. 
533 |a Microfiche.  |b [Washington, D.C. :  |c National Aeronautics and Space Administration,  |d 1994- ]  |e microfiche. 
650 0 |a Laser Doppler velocimeter.  |0 http://id.loc.gov/authorities/subjects/sh85074775. 
650 0 |a Rotors (Helicopters)  |x Aerodynamics.  |0 http://id.loc.gov/authorities/subjects/sh85115511. 
700 1 |a Mace, W. Derry. 
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