NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Wind-tunnel tests on the ground effectWind tunnel tests for prediction of ground effect on slender wing aircraft of low aspect ratio
Document ID
19670026813
Acquisition Source
Legacy CDMS
Document Type
Technical Translation (TT)
Authors
A. de Sievers
Date Acquired
September 2, 2013
Publication Date
July 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TT-F-11059
TN-87
Report Number: NASA-TT-F-11059
Report Number: TN-87
Accession Number
67N36142
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
WIND TUNNEL STABILITY TEST
GROUND EFFECT
SLENDER WING
ASPECT RATIO
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

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