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AviationAttack and Fighter Aircraft

An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes. Volume 2. Appendices 1 through 5

Authors: T. P. Neal; Rogers E. Smith; CORNELL AERONAUTICAL LAB INC BUFFALO NY
Abstract:
Contents: Pilot comments, bode plots, time histories for each configuration; Analysis of data using equivalent dynamics; Complete C* time histories; Longitudinal transfer functions; Details of simulation mechanization and data reduction techniques.

Limitations: APPROVED FOR PUBLIC RELEASE
Description: Final rept.
Pages: 175
Report Date: DEC 1970
Contract Number: F3361569C1664
Report Number: 0252088
Keywords relating to this report:
AERIAL WARFARE
DESIGN
DESIGN CRITERIA
FIGHTER AIRCRAFT
FLIGHT CONTROL SYSTEMS
FLIGHT TESTING
JET TRAINING PLANES
PITCH(MOTION)
SIMULATION
STABILITY
STANDARDS
STATISTICAL DATA
T-33 AIRCRAFT
VARIABLE STABILITY AIRCRAFT
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