Wind tunnel investigation of high lift capabilities of 2 supersonic configurations equipped with stowable, fabric wings of parachute like construction that may be used for takeoff and landing; use of parawing resulted in threefold increase in lift coefficient at aircraft attitude of 12°; static lateral stability characteristics of canard model were improved by adding parawing.
Exploratory study of parawing as high-lift device for aircraft
NASA -- Tech Note
1960
31 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1963
|Ultra-light competitive titanium alloy parawing aircraft
Europäisches Patentamt | 2020
|NTRS | 1963
|Large parawing development project
NTRS | 1967
|