NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
A method for predicting helicopter wake geometry, wake-induced flow and wake effects on blade airloadsWake model and computer program to compute geometries, flows and velocity influence coefficients for helicopter blade load calculations
Document ID
19710050392
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sadler, S. G.
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Publication Information
Publisher: AMERICAN HELICOPTER SOCIETY, INC.,
Subject Category
Aerodynamics
Report/Patent Number
AHS PREPRINT 523
Report Number: AHS PREPRINT 523
Meeting Information
Meeting: ANNUAL NATIONAL V/STOL FORUM
Location: WASHINGTON, DC
Start Date: May 19, 1971
End Date: May 21, 1971
Sponsors: AMERICAN HELICOPTER SOCIETY
Accession Number
71A31089
Funding Number(s)
CONTRACT_GRANT: NAS1-8448
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available