NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
The Effect on Stability and Control of a Pusher Propeller Behind Conventional Tail Surfaces as Determined by Tests of a Powered Model in the Free-flight Tunnel
Document ID
19930092561
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hollingworth, Thomas A
Date Acquired
September 6, 2013
Publication Date
January 1, 1943
Report/Patent Number
NACA-WR-L-220
Report Number: NACA-WR-L-220
Accession Number
93R21851
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPELLERS, PUSHER VS TRACTOR
STABILITY TESTS, WIND-TUNNEL
AIR FLOW - VISUALIZATION - TUFTS
WIND TUNNELS - NACA - FREE-FLIGHT (12') (AMER )
STABILITY & CONTROL
INSTABILITY, SPIRAL
AIRPLANES - TRIM
ENGINES, SUBMERGED
TAIL SURFACES - DESIGN
STABILITY, DIRECTIONAL

Related Records

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