Research Catalog

Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip

Title
Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip / William T. Yeager, Jr. [and four others].
Author
Yeager, William T.
Publication
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.

Available Online

https://purl.fdlp.gov/GPO/gpo65467

Details

Additional Authors
  • Langley Research Center, issuing body.
  • United States. National Aeronautics and Space Administration, sponsoring body.
Description
1 online resource (23 pages) : illustrations.
Series Statement
  • NASA technical memorandum ; 4754
  • ARL technical report ; 1283
Uniform Title
  • NASA technical memorandum ; 4754.
  • ARL-TR (Aberdeen Proving Ground, Md.) ; 1283.
Subjects
Note
  • Title from title screen (viewed on Feb. 19, 2016).
  • "May 1997."
  • "Performing organizations: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center; Joint Research Program Office, Aeroflightdynamics Directorate, U.S. Army Aviation and Troop Command, NASA Langley Research Center"Report documentation page.
  • "ATCOM technical report 97-A-006."
Bibliography (note)
  • Includes bibliographical references (page 6).
Funding (note)
  • Sponsored by the National Aeronautics and Space Administration
Call Number
GPO Internet NAS 1.15:4754
OCLC
marcive74226211
Author
Yeager, William T., author.
Title
Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip / William T. Yeager, Jr. [and four others].
Publisher
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA technical memorandum ; 4754
ARL technical report ; 1283
NASA technical memorandum ; 4754.
ARL-TR (Aberdeen Proving Ground, Md.) ; 1283.
Bibliography
Includes bibliographical references (page 6).
Funding
Sponsored by the National Aeronautics and Space Administration WU 05-63-36-02 PR A5008 L- 17558 NASA TM-4754 ARL-TR- 1283 ATCOM TR-97-A-006
Connect to:
https://purl.fdlp.gov/GPO/gpo65467
Added Author
Langley Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Other Form:
Print version: Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip (OCoLC)37002414
Microfiche version: Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip (OCoLC)40711867
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:4754
View in Legacy Catalog