Author

Harold H. Youngren

Observed names: H. H. Youngren, H. YOUNGREN, HAROLD YOUNGREN, Harold Youngren

Observed institutions: Lockheed (United States), Massachusetts Institute of Technology

OpenAlex ID: A5063482571

Body Freedom Flutter of High Aspect Ratio Flying Wings

2005 · Michael Love, P Zink, et al. · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 84

Autonomous Aerosondes for Economical Atmospheric Soundings Anywhere on the Globe

1992 · Greg J. Holland, Tad McGeer, et al. · Bulletin of the American Meteorological Society · 64

Viscous/inviscid method for preliminary design of transonic cascades

1991 · HAROLD YOUNGREN, MARK DRELA · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 63

Comparison of panel method formulations and its influence on the development of QUADPAN, an advanced low-order method

1983 · H. YOUNGREN, E. BOUCHARD, et al. · AIAA Applied Aerodynamics Conference · 41

Lockheed Martin's SAMARAI Nano Air Vehicle: Challenges, Research, and Realization

2012 · Steve Jameson, Kingsley Fregene, et al. · AIAA Aerospace Sciences Meeting · 29

Engineering Applications of an Advanced Low-Order Panel Method

1985 · C. E. Johnston, H. H. Youngren, et al. · SAE technical papers on CD-ROM/SAE technical paper series · 28

Analysis and design of transonic cascades with splitter vanes

1991 · Harold Youngren · DSpace@MIT (Massachusetts Institute of Technology) · 27

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Low Reynolds Number Testing of the AG38 Airfoil for the SAMARAI Nano Air Vehicle

2008 · Harold Youngren, Chris Kroninger, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 18

Control of Aerodynamic Flows. Delivery Order 0051: Transition Prediction Method Review Summary for the Rapid Assessment Tool for Transition Prediction (RATTraP)

2005 · Myron B. Davis, Helen Reed, et al. · Defense Technical Information Center (DTIC) · 12

Multi-Point Design and Optimization of an Natural Laminar Flow Airfoil for a Mission Adaptive Compliant Wing

2008 · Harold Youngren · AIAA Aerospace Sciences Meeting and Exhibit · 11

Test, Analysis and Design of Propeller Propulsion Systems for MAVs

2011 · Harold Youngren, Ming Chang · AIAA Aerospace Sciences Meeting · 9

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

2004 · Scott Zink, Michael Love, et al. · AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (MAO) · 9

Flight Research with the MIT Daedalus Prototype

1987 · Steven R. Bussolari, John S. Langford, et al. · SAE technical papers on CD-ROM/SAE technical paper series · 5

Design Optimization of America’s Cup AC75 Hydrofoil Sections with Flaps

2025 · Galen W. Ng, Anil Yildirim, et al. · Journal of Sailing Technology · 3

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CFD-Based Design Optimization of Subcavitating Hydrofoil Sections with Flaps

2025 · Anil Yildirim, Galen W. Ng, et al. · SNAME Chesapeake Sailing Yacht Symposium (CSYS) · 2

Configuration Study and Performance of a Military V/STOL Roadable Aircraft

2011 · Francesco Giannini, Antoine Deux, et al. · AIAA Aviation Technology, Integration, and Operations Conference (ATIO) · 1

Design of the Samaarai Monowing Rotorcraft Nano Air Vehicle

2009 · Harold Youngren, Steve Jameson, et al. · Vertical Flight Society Forum · 1

Mission Adaptive Compliant Wing, Flight Test Results/Future Applications

2008 · Sridhar Kota, Russell Osborn, et al. · AIAA Applied Aerodynamics Conference · 1

PVU: A Medium-Order Finite Element Panel Method

2026 · Mark Drela, Demet Ulker, et al. · AIAA SciTech Forum

Daedalus

2013 · Harold Youngren · American Institute of Aeronautics and Astronautics eBooks

Development and Flight Validation of an Autonomous Mono-Wing UAS

2010 · Kingsley Fregene, Steve Jameson, et al. · Vertical Flight Society Forum

Works count: 21

Citation count: 408

H-index: 10

I10-index: 10