Investigation of flying qualities of military aircraft at high angles of attack.
Volume I,
Technical results /
by Donald E. Johnson, Irving L. Ashkenas, Jeffrey R. Hogge.

Description

Main Author

Johnston, Donald E.

Related Names

Hogge, Jeffrey R., author.
Ashkenas, Irving L., author.
Air Force Flight Dynamics Laboratory (U.S.)
Systems Technology, Inc.

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974.

Subjects

Airplanes, Military.
Stalling (Aerodynamics)
Spin (Aerodynamics)
Angle of attack (Aerodynamics)

Summary

Attention has been focused on departure (e.g., nose slice, wing rock) and recovery of military aircraft as opposed to spin entry. The approach has been to analytically identify and validate key flying quality parameters, to qualitatively assess and verify these through piloted simulation, and to measure and quantify effects on key dynamic parameters of pilot describing functions.

Note

"June 1974."

Physical Description

xv, 143 pages : illustrations ; 28 cm.

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