Dynamic Stability Parameters

reportActive / Technical Report | Accession Number: ADA103764 | Open PDF

Abstract:

Contents Aerodynamic Mathematical Modeling - Basic Concepts Impact of High-Alpha Aerodynamics on Dynamic Stability Parameters of Aircraft and Missiles Review of Techniques for Determination of Dynamic Stability Parameters in Wind Tunnels Direct Forced-Oscillation Techniques for the Determination of Stability Derivatives in Wind-Tunnels Wind Tunnel Measurement of Aerodynamic Derivatives Using Flexible-Sting Rigs Rotary and Magnus Balances Curved-Flow, Rolling Flow and Oscillatory PUre-Yawing Wind-Tunnel Test Methods for Determination of Dynamic Stability Derivatives Support Interference Applications of Half-Model Technique in Dynamic Stability Testing Determination of Aircraft Dynamic Stability and Control Parameters from Flight Testing Estimation of Dynamic Stability Parameters from Drop Model Flight Tests Analytical Determination of Dynamic Stability Parameters Aeroelasticity, Including Dynamic Effects of Separated Flow Control Derivatives Sensitivity of Aircraft Motion to Cross-Coupling and Acceleration Derivatives Some Applications of Aerodynamic Formulations to Problems in Aircraft Dynamics Applications of Dynamic Stability Parameters to Problems in Aircraft Dynamics and Application to Missile Dynamics.

Author(s):
No Author(s) Identified
Author Organization(s):
ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)
Descriptive Note:
Lecture series
Supplementary Note:
Lecture series presented at NASA Ames Research Center, 2-5 Mar 81, Moffett Field, CA and von Karman Inst., 16-19 Mar 81 Rhode-Saint-Genese (Belgium). See also ADA063851.
Pagination:
0391

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release, Nato
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited. Nato.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AGARD-LS-114
Monitor Series:
AGARD
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning; JCA_1.1_Force Management; JCA_1_Force Support; JCA_5.3.1_Analyze Problem; JCA_4.6_Engineering; JCA_4.7.2_Installation Services; JCA_4.7_Base and Installations Support; JCA_4.6.1_General Engineering; JCA_1.2.7_Experimentation; JCA_5.2_Understand; JCA_5.3.2_Apply Situational Understanding; JCA_5.1.1_Establish and Maintain Unity of Effort with Mission Partners; JCA_5.1_Organize; JCA_5.3.4_Develop Courses of Action; JCA_5.3.5_Analyze Courses of Action; JCA_5.3.3_Develop Strategy; JCA_5.2.3_Share Knowledge and Situational Awareness; JCA_1.3.2_Personnel Management; JCA_1.2.6_Concepts; JCA_4.5.4_Requirements Definition
Modernization Areas:
Hypersonics
Communities of Interest:
Air Platforms
Descriptor(s):
*AERODYNAMIC STABILITY, *AIRCRAFT, *GUIDED MISSILES, FLIGHT TESTING, STABILITY, ROLL, PITCH(MOTION), YAW, ACCELERATION, DYNAMIC RESPONSE, ANGLE OF ATTACK, AEROELASTICITY, AERODYNAMIC CHARACTERISTICS, WIND TUNNEL TESTS, STING MOUNTS, FLIGHT MANEUVERS, OSCILLATION, FLOW SEPARATION, FLEXIBLE STRUCTURES, DYNAMIC TESTS, NATO, LECTURES, MATHEMATICAL MODELS, COUPLING(INTERACTION)
Field(s)/Group(s):
Aerodynamics, Aircraft, Guided Missile Dynamics, Configurations and Control Surfaces, Guided Missiles
Keyword(s):
*DYNAMIC STABILITY, NATO FURNISHED, HIGH ANGLES
Report Date:
1981 May 01