Accession Number:

AD0652998

Title:

METHODES UTILISEES POUR LA MISE AU POINT DE L'AVION BREGUET 940 A AILES SOUFFLEES (METHODS USED FOR THE FINAL DESIGN ANALYSIS OF THE BREGUET 940 'BLOWER-WING' PLANE),

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

• DERichemont,G.

Report Date:

1961-04-01

Pagination or Media Count:

25.0

Abstract:

Many coordinated methods were utilized in the study of the dynamic characteristics of the aircraft Breguet 940. Methods of study included utilization of a fixed model in a wind tunnel, a motorized flying model, an electronic flight simulator, and observations of the aircraft itself in flight.

Descriptors:

• *SHORT TAKEOFF AIRCRAFT
• AERODYNAMIC CHARACTERISTICS
• MODEL TESTS
• WIND TUNNEL MODELS
• FLIGHT TESTING
• FLIGHT SIMULATORS
• TRANSPORT AIRCRAFT
• FRANCE

Subject Categories:

• Aerodynamics
• Transport Aircraft
• VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE