Research Catalog

Induced inflow velocity and blade surface pressure measurements for a helicopter model in forward flight.

Title
Induced inflow velocity and blade surface pressure measurements for a helicopter model in forward flight. Volume 1, Advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 710 ft/sec [microform] / Joe W. Elliott ... [et al.].
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity, [1992]

Details

Additional Authors
  • Elliott, Joe W.
  • United States. Army Aviation Research and Technology Activity.
  • Langley Research Center.
Description
1 v.
Series Statement
  • NASA technical memorandum ; 104224
  • AVSCOM TR ; 92-B-003
Uniform Title
AVSCOM technical report ; 92-B-003.
Subject
  • Rotors (Helicopters) > Aerodynamics
  • Laser Doppler velocimeter
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 93-0939-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:104224
OCLC
marcive28918023
Title
Induced inflow velocity and blade surface pressure measurements for a helicopter model in forward flight. Volume 1, Advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 710 ft/sec [microform] / Joe W. Elliott ... [et al.].
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity, [1992]
Series
NASA technical memorandum ; 104224
AVSCOM TR ; 92-B-003
AVSCOM technical report ; 92-B-003.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993 5 microfiches.
Added Author
Elliott, Joe W.
United States. Army Aviation Research and Technology Activity.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:104224
Research Call Number
READEX Microfiche NAS 1.15:104224
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