NASA-TN-D-3437
Investigation of a semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control in hovering
Year: 1966
Abstract: Hovering force-test on semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control
Subject: AERODYNAMICS
Show full item record
contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
date accessioned | 2017-09-04T18:50:25Z | |
date available | 2017-09-04T18:50:25Z | |
date copyright | 06/01/1966 | |
date issued | 1966 | |
identifier other | KUTKAEAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/231874 | |
description abstract | Hovering force-test on semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control | |
language | English | |
title | NASA-TN-D-3437 | num |
title | Investigation of a semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control in hovering | en |
type | standard | |
page | 76 | |
status | Active | |
tree | NASA - National Aeronautics and Space Administration (NASA):;1966 | |
contenttype | fulltext | |
subject keywords | AERODYNAMICS | |
subject keywords | AIRCRAFT | |
subject keywords | EFFECT | |
subject keywords | FLAPPING | |
subject keywords | GROUND | |
subject keywords | HOVERING | |
subject keywords | MODEL | |
subject keywords | MODELS | |
subject keywords | SEMISPAN | |
subject keywords | TAKEOFF | |
subject keywords | TILT | |
subject keywords | VERTICAL | |
subject keywords | VTOL | |
subject keywords | WING | |
subject keywords | YAW |