Research Catalog

Parametric tip effects for conformable rotor applications

Title
Parametric tip effects for conformable rotor applications [microform] / Wayne R. Mantay, William T. Yeager, Jr.
Author
Mantay, Wayne R.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]

Details

Additional Authors
  • Yeager, William T.
  • United States. Army Aviation Research and Development Command.
  • Langley Research Center.
Description
1 v.
Series Statement
  • NASA technical memorandum ; 85682
  • USAAVRADCOM TR ; 83-B-4
Uniform Title
  • AVRADCOM technical report ; 83-B-4.
  • NASA technical memorandum ; 85682.
Subject
  • Aeroelasticity
  • Blade tips
  • Helicopters
  • Rotary wings
  • Rotor aerodynamics
  • Wind tunnel tests
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.15:85682
OCLC
marcive244475177
Author
Mantay, Wayne R.
Title
Parametric tip effects for conformable rotor applications [microform] / Wayne R. Mantay, William T. Yeager, Jr.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
Series
NASA technical memorandum ; 85682
USAAVRADCOM TR ; 83-B-4
AVRADCOM technical report ; 83-B-4.
NASA technical memorandum ; 85682.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration]. 1983. 1 microfiche.
Added Author
Yeager, William T.
United States. Army Aviation Research and Development Command.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:85682
Research Call Number
GPO Microfiche NAS 1.15:85682
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