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
Analysis of wing slipstream flow interactionTheoretical analysis of wing lift in wide and circular stripstreams, and engineering method for predicting practical V/STOL configuration characteristics
Document ID
19700027535
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jameson, A. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
August 5, 2013
Publication Date
August 1, 1970
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-1632
Report Number: NASA-CR-1632
Accession Number
70N36851
Funding Number(s)
CONTRACT_GRANT: NAS2-4658
Distribution Limits
Public
Copyright
Other

Related Records

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