Accession Number:

ADA101646

Title:

Investigation of High-Angle-of-Attack Maneuver-Limiting Factors. Part 1. Analysis and Simulation

Descriptive Note:

Final rept. 13 May 1976-30 Jul 1980

Corporate Author:

SYSTEMS TECHNOLOGY INC HAWTHORNE CA

Personal Author(s):

• Johnston, Donald E.
• Mitchell, David G.
• Myers, Thomas T.

Report Date:

1980-12-01

Pagination or Media Count:

203.0

Abstract:

The high-angle-of-attack, low-speed stalldeparture characteristics of the F-4J and F-14A are analyzed, using a six-degree-of-freedom mathematical model with nonlinear aerodynamics. Cause-effect relationships are investigated for maneuver limiting factors including wing rock, nose slice, and rolling departures. Cross-derivatives of L alpha, N alpha, and M beta alter key transfer function parameters. A piloted simulation validates analytic predictions and demonstrates that departure warning, susceptibility, and severity are strongly influenced by the static cross-derivatives. A connection between roll numerator parameter values and pilot perception of departure susceptibility and severity is identified. Potential modifications for the high AOA sections of the MIL-F- 8785B Flying Qualities Specification are proposed a criterion for the real part of the roll numerator root, further recommendations for minimizing departure susceptibility and certain sideslip influences, and a flying quality rating form for assessing departure and recovery characteristics. Part I, Analysis and Simulation, presents a summary of the complete investigation and results. Part II, Piloted Simulation Assessment of Bihrle Departure Criteria, presents a detailed comparison of analytical prediction and piloted simulation results for a specific set of programmed control deflections. Part III, Appendices -- Aerodynamic Models, contains the detailed aerodynamic models employed in the F- 4J and F-14A high-angle-of-attack analysis and validation and the equations of motion, aerodynamic models, control system configurations, etc., employed in the piloted simulation.

Descriptors:

• *MATHEMATICAL MODELS
• *AIRCRAFT
• *PERFORMANCE(ENGINEERING)
• *JET FIGHTERS
• RECOVERY
• TRANSFER FUNCTIONS
• EQUATIONS OF MOTION
• PARAMETERS
• MATRICES(MATHEMATICS)
• DEFLECTION
• ANGLE OF ATTACK
• LOW VELOCITY
• STALLING
• NONLINEAR SYSTEMS
• MATHEMATICAL PREDICTION
• AERODYNAMIC CHARACTERISTICS
• SIDESLIP
• CLOSED LOOP SYSTEMS

Subject Categories:

• Attack and Fighter Aircraft
• Theoretical Mathematics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE