Michael H. Love

发表

Body Freedom Flutter of High Aspect Ratio Flying Wings

Paul Scott Zink, Michael H. Love, Paul Wieselmann, 2005 .

Demonstration of Morphing Technology through Ground and Wind Tunnel Tests

David White, Paul Scott Zink, Michael H. Love, 2007 .

Impact of Active Aeroelastic Wing Technology on Wing Geometry Using Response Surface Methodology

Dimitri N. Mavris, Paul Scott Zink, Michael H. Love, 1999 .

A Methodology of Large Scale Computational Aeroelasticity for the MDA/MDO Environment

Lockheed Martin, Michael H. Love, R. Kolonay, 2000 .

The Impact of Unsteady Aerodynamics on the Loading of Flight Vehicles

Antonio De La Garza, Michael H. Love, 2005 .

Robust Design for Aeroelastically Tailored/Active Aeroelastic Wing

Dimitri N. Mavris, Mordechay Karpel, Paul Scott Zink, 1998 .

GLA and Flutter Suppression for a SensorCraft Class Concept Using System Identification

Antonio De La Garza, Paul Scott Zink, Michael H. Love, 2008 .

Development of Wing Structural Weight Equation for Active Aeroelastic Wing Technology

Dimitri N. Mavris, Michael H. Love, P. Scott Zink, 1999 .

The Impact of Active Aeroelastic Wing Technology on Conceptual Aircraft Design

Paul Scott Zink, Michael H. Love, Peter M. Flick, 2000 .

Validation of the Lockheed Martin Morphing Concept with Wind Tunnel Testing

Terrence A. Weisshaar, Robert C. Scott, Michael H. Love, 2007 .

STRUCTURAL OPTIMIZATION WITH STRESS AND AEROELASTIC CONSTRAINTS USING EXPANDABLE MODAL BASIS

Lockheed Martin, Mordechay Karpel, Michael H. Love, 1998 .

Drag Minimization Through the Use of Mission Adaptive Trailing Edge Flaps and Fuel State Control

Michael H. Love, Harold Youngren, P. Scott Zink, 2004 .