The Resource 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, Joe W. Elliott ... [and others]

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, Joe W. Elliott ... [and others]

Label
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
Title
Induced inflow velocity and blade surface pressure measurements for a helicopter model in forward flight
Title number
Volume 1
Title part
Advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 710 ft/sec
Statement of responsibility
Joe W. Elliott ... [and others]
Contributor
Subject
Language
eng
Member of
Cataloging source
GPO
Government publication
federal national government publication
Index
no index present
Literary form
non fiction
http://library.link/vocab/relatedWorkOrContributorName
  • Elliott, Joe W
  • United States
  • Langley Research Center
Series statement
  • AVSCOM TR
  • NASA technical memorandum
Series volume
  • 92-B-003
  • 104224
http://library.link/vocab/subjectName
  • Rotors (Helicopters)
  • Laser Doppler velocimeter
Label
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, Joe W. Elliott ... [and others]
Instantiates
Publication
Note
  • Distributed to depository libraries in microfiche
  • Shipping list no.: 93-0939-M
Carrier category
microfiche
Carrier category code
he
Carrier MARC source
rdacarrier
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Control code
17196742
Extent
1 volume.
Form of item
microfiche
Media category
microform
Media MARC source
rdamedia
Media type code
h
Reproduction note
Microfiche.
Stock number
N 93-24532
Label
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, Joe W. Elliott ... [and others]
Publication
Note
  • Distributed to depository libraries in microfiche
  • Shipping list no.: 93-0939-M
Carrier category
microfiche
Carrier category code
he
Carrier MARC source
rdacarrier
Content category
text
Content type code
txt
Content type MARC source
rdacontent
Control code
17196742
Extent
1 volume.
Form of item
microfiche
Media category
microform
Media MARC source
rdamedia
Media type code
h
Reproduction note
Microfiche.
Stock number
N 93-24532

Library Locations

    • Indiana State LibraryBorrow it
      315 W. Ohio St., Indianapolis, IN, 46202, US
      39.77004 -86.164015

Library Links

Processing Feedback ...