Subject: (39) Structural Mechanics
Number of records: 69.
Jenkins, Jerald M. (1988) A Comparison of Experimental and Calculated Thin-Shell Leading-Edge Buckling Due to Thermal Stress. Technical Report NASA TM-100416, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Taylor, Allan H. and Sakata, I. Frank (1985) A Comparison of Measured and Calculated Thermal Stresses in a Hybrid Metal Matrix Composite Spar Cap Element. Technical Report NASA TM-86729, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1966) A Pretensioning Concept for Relief of Critical Leading-Edge Thermal Stress. Technical Report NASA Technical Note TN D-3507, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Kuhl, Albert E. (1977) A Study of the Effect of Radical Load Distributions on Calibrated Strain Gage Load Equations. Technical Report NASA TM-56047, Research Engineering, NASA Dryden Flight Research Center.
Martin, C. Wayne and Lung, S. F. and Gupta, K. K. (1989) A Three-Node C° Element for Analysis of Laminated Composite Sandwich Shells. Technical Report NASA TM-4125, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1987) Accuracies of Southwell and Force/Stiffness Methods in the Prediction of Buckling Strength of Hypersonic Aircraft Wing Tubular Panels. Technical Report NASA TM-88295, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (2003) Aging Theories for Establishing Safe Life Spans of Airborne Critical Structural Components. Technical Report NASA/TP-2003-212034, Research Engineering, NASA Dryden Flight Research Center.
Richards, W. Lance and Monaghan, Richard C. (1996) Analytical and Experimental Verification of a Flight Article for a Mach-8 Boundary-Layer Experiment. Technical Report NASA TM-4733, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1998) Anomalous Buckling Characteristics of Laminated Metal-Matrix Composite Plates with Central Square Holes. Technical Report NASA/TP-1998-206559, Research Engineering, NASA Dryden Flight Research Center.
Ko, W.L. and Carter, A.L. and Totton, W.W. and Ficke, J.M. (1989) Application of Fracture Mechanics and Half-Cycle Method to the Prediction of Fatigue Life of B-52 Aircraft Pylon Components. Technical Report NASA TM-88277, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Richards, W. Lance and Fleischer, Van Tran (2009) Applications of Ko Displacement Theory to the Deformed Shape Predictions of the Doubly-Tapered Ikhana Wing. Technical Report NASA TP-2009-214652, Research and Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Shideler, John L. and Fields, Roger A. (1986) Buckling Behavior of Rene 41 Tubular Panels for a Hypersonic Aircraft Wing. Technical Report NASA TM-86798, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jackson, Raymond H. (1991) Combined Compressive and Shear Buckling Analysis of Hypersonic Aircraft Structural Sandwich Panels. Technical Report NASA TM-4290, Research Engineering, NASA Dryden Flight Research Center.
Fields, Roger A. and Richards, W. Lance and DeAngelis, V. Michael (2004) Combined Loads Test Fixture for Thermal-Structural Testing Aerospace Vehicle Panel Concepts. Technical Report NASA/TM-2004-212039, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jackson, Raymond H. (1991) Combined-Load Buckling Behavior of Metal-Matrix Composite Sandwich Panels Under Different Thermal Environments. Technical Report NASA TM-4321, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1987) Comparison of Measured Temperatures, Thermal Stresses and Creep Residues With Predictions on a Built-up Titanium Structure. Technical Report NASA TM-86814, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1980) Comparison of Structural Behavior of Superplastically Formed/Diffusion-Bonded Sandwich Structures and Honeycomb Core Sandwich Structures. Technical Report NASA TM-81348, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jackson, Raymond H. (1993) Compressive and Shear Buckling Analysis of Metal Matrix Composite Sandwich Panels Under Different Thermal Environments. Technical Report NASA TM-4492, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jackson, Raymond H. (1991) Compressive Buckling Analysis of Hat-Stiffened Panel. Technical Report NASA TM-4310, Research Engineering, NASA Dryden Flight Research Center.
Nissim, E. and Burken, John J. (1988) Control Surface Spanwise Placement in Active Flutter Suppression Systems. Technical Report NASA TP-2873, Research Engineering, NASA Dryden Flight Research Center.
Kehoe, Michael W. and Deaton, Vivian C. (1993) Correlation of Analytical and Experimental Hot Structure Vibration Results. Technical Report NASA TM-104269, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (2004) Debonding Stress Concentrations in a Pressurized Lobed Sandwich-Walled Generic Cryogenic Tank. Technical Report NASA/TP-2004-212849, Research Engineering, NASA Dryden Flight Research Center.
Nissim, E. (1990) Design of Control Laws for Flutter Suppression Based on the Aerodynamic Energy Concept and Comparisons With Other Design Methods. Technical Report NASA TP-3056, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Richards, W.L. and Tran, Van T. (2007) Displacement Theories for In-Flight Deformed Shape Predictions of Aerospace Structures. Technical Report NASA/TP-2007-214612, Research and Engineering, NASA Dryden Flight Research Center.
Nissim, E. (1989) Effect of Control Surface Mass Unbalance on the Stability of a Closed-Loop Active Control System. Technical Report NASA TP-2952, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1984) Effect of Creep in Titanium Alloy Ti-6A1-4V at Elevated Temperature on Aircraft Design and Flight Test. Technical Report NASA TM-86033, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1980) Elastic Constants for Superplastically Formed/Diffusion-Bonded Corrugated Sandwich Core. Technical Report NASA TP-1562, Research Engineering, NASA Dryden Flight Research Center.
Reardon, Lawrence F. (1989) Evaluation of a Strain-Gage Load Calibration on a Low-Aspect-Ratio Wing Structure at Elevated Temperature. Technical Report NASA TP-2921, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Montoya, Christopher A. (1983) Experimental Creep Data for a Built-up Aluminum/Titanium Structure Subjected to Heating and Loading. Technical Report NASA TM-84906, Research and Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Chen, Tony (2006) Extended Aging Theories for Predictions of Safe Operational Life of Critical Airborne Structural Components. Technical Report NASA/TP-2006-213676, Research Engineering, NASA Dryden Flight Research Center.
Richards, W. Lance (1997) Finite-Element Analysis of a Mach-8 Flight Test Article Using Nonlinear Contact Elements. Technical Report NASA TM-4796, Research Engineering, NASA Dryden Flight Research Center.
Tang, Ming H. and Pearson, George P. E. (1971) Flight-Measured HL-10 Lifting Body Center Fin Loads and Control Surface Hinge Moments and Correlation With Wind-Tunnel Predictions. Technical Report NASA TM X-2419, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Fleischer, Van Tran (2009) Further Development of Ko Displacement Theory for Deformed Shape Predictions of Non-uniform Aerospace Structures. Technical Report NASA TP-2009-214643, Research and Engineering, NASA Dryden Flight Research Center.
Ko, William L. (2004) Heat Shielding Characteristics and Thermostructural Performance of a Superalloy Honeycomb Sandwich Thermal Protection System (TPS). Technical Report NASA/TP-2004-212024, Research Engineering, NASA Dryden Flight Research Center.
Gupta, Kajal K. and Lawson, Charles L. (1987) Implementation of a Block Lanczos Algorithm for Eigenproblem Solution of Gyroscopic Systems. Technical Report NASA TM-88290, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Tran, Van T. and Chen, Tony (2007) Incorporation of Half-Cycle Theory Into Ko Aging Theory for Aerostructural Flight-Life Predictions. Technical Report NASA/TP-2007-214608, Research and Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1987) Inelastic Strain Analogy for Piecewise Linear Computation of Creep Residues in Built-up Structures. Technical Report NASA TM-86813, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1993) Mechanical and Thermal Buckling Analysis of Sandwich Panels Under Different Edge Conditions. Technical Report NASA TM-4535, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1998) Mechanical- and Thermal-Buckling Behavior of Rectangular Plates With Different Central Cutouts. Technical Report NASA/TM-1998-206542, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1999) Open-Mode Debonding Analysis of Curved Sandwich Panels Subjected to Heating and Cryogenic Cooling on Opposite Faces. Technical Report NASA/TP-1999-206580, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Monaghan, Richard C. and Jackson, Raymond H. (1992) Practical Theories for Service Life Prediction of Critical Aerospace Structural Components. Technical Report NASA TM-4354, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1987) Prediction of Service Life of Aircraft Structural Components Using the Half-Cycle Method. Technical Report NASA TM-86812, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1995) Predictions of Thermal Buckling Strengths of Hypersonic Aircraft Sandwich Panels Using Minimum Potential Energy and Finite Element Methods. Technical Report NASA TM-4643, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Schuster, Lawrence S. (1984) Preflight Transient Dynamic Analyses of B-52 Aircraft Carrying Space Shuttle Solid Rocket Booster Drop-Test Vehicle. Technical Report NASA TM-84925, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jackson, Raymond H. (1994) Shear Buckling Analysis of a Hat-Stiffened Panel. Technical Report NASA TM-4644, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. (2007) Six Decades of Flight Research: An Annotated Bibliography of Technical Publications of NASA Dryden Flight Research Center, 1946-2006. Technical Report NASA/TP-2007-213684, Research and Engineering, NASA Dryden Flight Research Center.
Gupta, K.K. (1984) STARS - A General-Purpose Finite Element Computer Program for Analysis of Engineering Structures. Technical Report NASA RP-1129, Research Engineering, NASA Dryden Flight Research Center.
Gupta, K.K. (1991) STARS – An Integrated General-Purpose Finite Element Structural, Aeroelastic, and Aeroservoelastic Analysis Computer Program. Technical Report NASA TM-101709 (Revised), Research Engineering, NASA Dryden Flight Research Center.
Gupta, K. K. (1997) STARS—An Integrated, Multidisciplinary, Finite-Element, Structural, Fluids, Aeroelastic, and Aeroservoelastic Analysis Computer Program. Technical Report NASA TM-4795, Research Engineering, NASA Dryden Flight Research Center.
Hanson, Curtis E. (2009) Static Aeroelastic Effects of Formation Flight for Slender Unswept Wings. Technical Report NASA/TM-2009-214649, Research and Engineering, NASA Dryden Flight Research Center.
Richards, W. Lance (1993) Strain Gage Measurement Errors in the Transient Heating of Structural Components. Technical Report NASA TM-104274, Research Engineering, NASA Dryden Flight Research Center.
Nelson II, Sigurd A. (1994) Strain-Gage Selection in Loads Equations Using a Genetic Algorithm. Technical Report NASA CR-4597, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Schuster, Lawrence S. (1985) Stress Analyses of B-52 Pylon Hooks. Technical Report NASA TM-84924, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1997) Stress Analysis of B-52 Pylon Hooks for Carrying the X-38 Drop Test Vehicle. Technical Report NASA/TM-97-206218, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (2005) Stress Analysis of B-52B and B-52H Air-Launching Systems Failure-Critical Structural Components. Technical Report NASA/TP-2005-212862, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (2005) Structural Analysis of Helios Filament-Wound Tanks Subjected to Internal Pressure and Cooling. Technical Report NASA/TM-2005-212855, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Kuhl, Albert E. and Carter, Alan L. (1977) The Use of a Simplified Structural Model as an Aid in the Strain Gage Calibration of a Complex Wing. Technical Report NASA TM 56046, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1996) Thermal and Mechanical Buckling Analysis of Hypersonic Aircraft Hat-Stiffened Panels with Varying Face Sheet Geometry and Fiber Orientation. Technical Report NASA TM-4770, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jackson, Raymond H. (1991) Thermal Behavior of a Titanium Honeycomb-Core Sandwich Panel. Technical Report NASA TM-101732, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (2004) Thermal Buckling Analysis of Rectangular Panels Subjected to Humped Temperature Profile Heating. Technical Report NASA/TP-2004-212041, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Fields, Roger A. (1987) Thermal Stress Analysis of Space Shuttle Orbiter Subjected to Reentry Aerodynamic Heating. Technical Report NASA TM-88286, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Jenkins, Jerald M. (1987) Thermal Stress Analysis of Space Shuttle Orbiter Wing Skin Panel and Thermal Protection System. Technical Report NASA TM-88276, Research Engineering, NASA Dryden Flight Research Center.
Thompson, Randolph C. and Richards, W. Lance (1991) Thermal-Structural Panel Buckling Tests. Technical Report NASA TM-104243, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1994) Thermocryogenic Buckling and Stress Analyses of a Partially Filled Cryogenic Tank Subjected to Cylindrical Strip Heating. Technical Report NASA TM-4579, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Gong, Leslie (2000) Thermoelastic Analysis of Hyper-X Camera Windows Suddenly Exposed to Mach 7 Stagnation Aerothermal Shock. Technical Report NASA/TP-2000-209030, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. and Gong, Leslie (2001) Thermostructural Analysis of Unconventional Wing Structures of a Hyper-X Hypersonic Flight Research Vehicle for the Mach 7 Mission. Technical Report NASA/TP-2001-210398, Research Engineering, NASA Dryden Flight Research Center.
Ko, William L. (1997) Thermostructural Behavior of a Hypersonic Aircraft Sandwich Panel Subjected to Heating on One Side. Technical Report NASA TM-4769, Research Engineering, NASA Dryden Flight Research Center.
Richards, W. Lance and Thompson, Randolph C. (1996) Titanium Honeycomb Panel Testing. Technical Report NASA-TM-4768, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. and Tang, Ming H. and Pearson, George P.E. (1968) Vertical-Tail Loads and Control-Surface Hinge-Moment Measurements on the M2-F2 Lifting Body During Initial Subsonic Flight Tests. Technical Report NASA TM X-1712, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Sat Nov 21 18:15:42 PST 2009.
