1983-02-01

Devices for Improvement of Controllability at Stall 830723

The stall characteristics of Learjet aircraft are discussed in terms of the aerodynamic phenomena which determine the stall behavior. A number of devices are described which have been flight tested in attempting to improve controllability at stall. Theories are offered to explain the effects of each device. Wind tunnel test data are compared with some of the flight results.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 16% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Aerodynamic Design Approach to the Stall/Spin Problem - The VariViggen

740391

View Details

TECHNICAL PAPER

Engineering Solutions for Circulation Control Applications

2005-01-3193

View Details

TECHNICAL PAPER

Gulfstream II Aerodynamic Design

670242

View Details

X