User's Manual for the Martin-Marietta High Angle of Attack Aerodynamic Methodology for Body Tail Missiles.

reportActive / Technical Report | Accession Number: ADA057138 | Open PDF

Abstract:

This report documents the computer program developed by the Army to evaluate and implement an aerodynamic methodology developed by the Martin Marietta Corporation. The methodology was developed to predict aerodynamic forces on slender missile bodies with low aspect ratio tails at low and high angles of attack, at arbitrary roll angles for both transonic and supersonic velocities. Author

Author(s):
Winn, Gary C.
Author Organization(s):
ARMY MISSILE RESEARCH AND DEVELOPMENT COMMAND REDSTONE ARSENAL AL TECHNOLOGY LAB
Descriptive Note:
Technical rept.,
Pagination:
0081

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release, Document Partially Illegible
Distribution Statement:
Availability: Document Partially Illegible.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
DRDMI-T-78-63
 Subject Terms
Joint Capability Areas:
JCA_7.2.1_Mitigate Lethal Effects; JCA_7.2_Mitigate; JCA_7_Protection; JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_5_Command and Control; JCA_5.3_Planning
Communities of Interest:
Weapons Technologies
Descriptor(s):
*COMPUTER PROGRAM DOCUMENTATION, *SLENDER BODIES, *AERODYNAMIC FORCES, COMPUTER PROGRAMS, AERODYNAMIC CONFIGURATIONS, ROLL, TAIL ASSEMBLIES, ANGLE OF ATTACK, MATHEMATICAL PREDICTION, AERODYNAMIC CHARACTERISTICS, SUPERSONIC FLOW, SUBROUTINES, ASPECT RATIO, TRANSONIC FLOW
Field(s)/Group(s):
Computer Programming and Software, Guided Missiles, Fluid Mechanics
Report Date:
1978 Jun 01