Research Catalog

Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90

Title
Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / Kevin W. Noonan and Gene J. Bingham.
Author
Noonan, Kevin W.
Publication
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.

Available Online

https://purl.fdlp.gov/GPO/gpo71094

Details

Additional Authors
  • Bingham, Gene J.
  • Langley Research Center.
  • United States. Army Aviation Research and Development Command.
  • Army Research and Technology Laboratories (U.S.). Structures Laboratory.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Description
1 online resource (82 pages) : chiefly illustrations.
Series Statement
  • NASA technical paper ; 1701
  • AVRADCOM technical report ; 80-B-5
Uniform Title
  • NASA technical paper ; 1701.
  • AVRADCOM technical report ; 80-B-5.
Subject
  • Aerodynamic characteristics
  • Airfoils
  • Helicopters
  • Reynolds number
  • Wind tunnel tests
  • Aerofoils > Testing
  • Helicopters > Aerodynamics
  • Rotors (Helicopters) > Testing
Note
  • Title from title screen (viewed on Aug. 16, 2016).
  • "September 1980."
  • "Performing Organization: NASA Langley Research Center and Structures Laboratory, AVRADCOM Research and Technolocy Laboratories"--Report documentation page.
Bibliography (note)
  • Includes bibliographical references (page 13).
Type of Report (note)
  • Technical paper.
Funding (note)
  • National Aeronautics and Space Administration and U.S. Army Aviation Research and Development Command
Call Number
GPO Internet NAS 1.60:1701
OCLC
marcive785231998
Author
Noonan, Kevin W., author.
Title
Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / Kevin W. Noonan and Gene J. Bingham.
Publisher
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA technical paper ; 1701
AVRADCOM technical report ; 80-B-5
NASA technical paper ; 1701.
AVRADCOM technical report ; 80-B-5.
Bibliography
Includes bibliographical references (page 13).
Type Of Report
Technical paper.
Funding
National Aeronautics and Space Administration and U.S. Army Aviation Research and Development Command 505-31-33-02
L-13139
Connect to:
https://purl.fdlp.gov/GPO/gpo71094
Added Author
Bingham, Gene J., author.
Langley Research Center.
United States. Army Aviation Research and Development Command.
Army Research and Technology Laboratories (U.S.). Structures Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Other Form:
Print version: Noonan, Kevin W. Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 (OCoLC)7363586
Microfiche version: Noonan, Kevin W. Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 (OCoLC)711544725
Gpo Item No.
0830-H-15 (online)
Sudoc No.
NAS 1.60:1701
View in Legacy Catalog