Experimental Missile Pitch- and Moll-Damping Characteristics at Large
Author:
Affiliation:
1. ARO, Inc., Arnold Air Force Station, Tenn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57188
Reference8 articles.
1. Test Mechanism for Measuring Pitch-Damping Derivatives of Missile Configurations at High Angles of Attack
2. Experimental Roll-Damping, Magnus, and Static-Stability Characteristics of Two Slender Missile Configurations at High Angles of Attack (0 to 90 deg) and Mach Numbers 0.2 through 2.5
3. THE AERODYNAMIC PROPERTIES OF A SIMPLE NON ROLLING FINNED CONE-CYLINDER CONFIGURATION BETWEEN MACH NUMBERS 1.0 AND 2.5
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