F-14(A) High Angle-of-Attack Flying Characteristics Reel 2 · Part 14

Description

The original agency catalog description reads: Audience: Aviators, R10 F-14(A), Aircrew F-14(A). Synopsis: The F-14(A) aircraft's high angle-of-attack flight regime is discussed in detail. The following topics are covered: adverse yaw, the effect of sideslip, the dihedral effect, directional stability, inertial and kinematic coupling, and the contribution of stores. Normal high angle-of-attack flying qualities are discussed, including stall recognition, loss of control effectiveness, and wing rock phenomena. The second half of the discussion covers departure recovery procedures induced by nose-high/low-airspeed, asymmetric thrust, coupling, and flight control inputs. Purpose: Familiarize aircrew with high angle-of-attack flying qualities of F-14(A) aircraft. F-14 F.R.S. replacement air group (RAG) syllabus.

Collection

Records of the Office of the Secretary of Defense

Series

Motion Picture Films and Video Recordings on Five Decades of U.S. Military Activities Around the World