Comparison of preliminary designs of stiffened panels optimized using PANDA2 for reusable launch vehicle propellant tanks

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 1, Issue III, 2000, Pages 1554-1585

  Lamberti, Luciano ^a   Venkataraman, Satchi ^a   Haftka, Raphael T ^a   Johnson, Theodore F ^a  

^a UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AIRCRAFT FUEL TANKS; APPROXIMATION THEORY; COMPUTER SIMULATION; COMPUTER SOFTWARE; FAILURE ANALYSIS; FINITE ELEMENT METHOD; OPTIMIZATION; SENSITIVITY ANALYSIS; STRUCTURAL PANELS;

LIQUID HYDROGEN TANK; REUSABLE LAUNCH VEHICLES; SOFTWARE PACKAGE PANDA2;

CATAPULTS (AIRCRAFT LAUNCHERS);

EID: 0033671680     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (57)