Volume II. Flying Qualities Phase. Chapter 9: Roll Coupling.

Volume II. Flying Qualities Phase. Chapter 9: Roll Coupling.

Active / Technical Report | Accession Number: ADA319980 |

Abstract:

Divergence experienced during rolling maneuvers has frequently been referred to as inertial coupling. This leads to a misconception of the problems involved. The divergence experienced during rolling maneuvers is complex because it involves not only inertial properties, but aerodynamic ones as well. The material in this chapter is intended to offer a physical explanation of the more important causes of roll coupling.

Author(s):

No Author(s) Identified

Author Organization(s):

AIR FORCE TEST PILOT SCHOOL EDWARDS AFB CA

Supplementary Note:

ADA319971 ADA319972 ADA319973 ADA319974 ADA319975 ADA319976 ADA319977 ADA319978 ADA319979 ADA319981 ADA319982 ADA319983 ADA319984 ADA319985 DOI: 10.21236/ADA319980

Pagination:

0024

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release

RECORD

Collection: TR

Identifying Numbers

Monitor Series:

USAF-TPS

Subject Terms

Joint Capability Areas:

JCA_5.3_Planning; JCA_5_Command and Control; JCA_3.2_Engagement; JCA_3_Force Application; JCA_1_Force Support; JCA_3.2.1_Kinetic Means

Modernization Areas:

Quantum Science and Computing

Communities of Interest:

Air Platforms

Descriptor(s):

*FLIGHT MANEUVERS, COUPLING(INTERACTION), PITCH(MOTION), YAW, INERTIA, EQUATIONS OF MOTION, AERODYNAMIC STABILITY, ANGLE OF ATTACK, AERODYNAMIC LOADING, SIDESLIP, FLIGHT PATHS

Field(s)/Group(s):

Aerodynamics

Report Date:

1989 Apr 01

Creation Date:

1997 Jan 29