Accession Number:

AD0745366

Title:

Users Manual for Tilt-Wing and Deflected Slipstream Aerodynamics Program,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/CONVAIR SAN DIEGO CALIF

Personal Author(s):

• Pederson,S. K.

Report Date:

1970-05-28

Pagination or Media Count:

54.0

Abstract:

A digital computer program was developed for the purpose of estimating the aerodynamic lift, longitudinal forces and pitching moment characteristics of a tilt-wing or deflected slip-stream VSTOL configuration. Punched card output from this program provides the aerodynamic input data to the performance program for calculating takeoffs, landings and transitions of VSTOL aircraft. Author

Descriptors:

• (*TILT WINGS
• AERODYNAMIC CHARACTERISTICS)
• SHORT TAKEOFF AIRCRAFT
• LIFT
• PITCH(MOTION)
• ANGLE OF ATTACK
• CONTROL SEQUENCES
• COMPUTER PROGRAMS

Subject Categories:

• Aerodynamics
• VSTOL
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE