Some Stability Problems of Vertically Rising Aircraft

SM_WF_1955-4309

9/21/1955

Authors
Abstract
Content

In recent years the reductions of weight, frontal area, and. bulk per horsepower of aircraft power plants have made it possible, and. probably economically feasible, to build. high-speed. aircraft which can take off and land. without forward speed. The Langley Laboratory of the NACA has been investigating the low speed and hovering stability and controllabi1ity of possibly suitable configurations for several years, in order to make available when needed adequate research information for the guidance of engineers and designers.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM_WF_1955-4309
Citation
Zimmerman, C., "Some Stability Problems of Vertically Rising Aircraft," Western Forum 1955, Los Angeles, California, September 21, 1955, https://doi.org/10.4050/SM_WF_1955-4309.
Additional Details
Publisher
Published
9/21/1955
Product Code
SM_WF_1955-4309
Content Type
Technical Paper
Language
English