← LeaderboardsInvestigatorsiAttributed = a PI's even-split share of each grant — a $1M grant with 2 PIs counts $500K each.
Continuum Dynamics Inc
$9,617,836
Total funding
11
Grants
Funding over time
peak $3M · FY2010–25$5M$3.8M$2.5M$1.3M$0
'10
'11
'12
'13
'14
'15
'16
'17
'18
'19
'20
'21
'22
'23
'24
'25
Funding mix
By agency
DOE$9,609,472 · 10
NASA$8,364 · 1
By mechanism
—$9,617,836 · 11
Investigators at Continuum Dynamics Inc
InvestigatorsiAttributed = a PI's even-split share of each grant — a $1M grant with 2 PIs counts $500K each.
Exposure= the full size of every grant they're on ($1M each).
Rising Stars
First grant in the last 5 yrs
Not enough data
Emerging Leaders
6–10 yrs in
Not enough data
All-Time
Most funded here, all years
Not enough data
Largest grants
ADVANCED METHODS FOR EFFICIENT AEROELASTIC ANALYSIS OF WIND TURBINES AND WIND FARMS$2,898,844
· FY2020 · Department of Energy
HARDENING ADVANCED METHODS FOR PREDICTING 3D UNSTEADY FLOWS AROUND WIND TURBINES FOR INDUSTRIAL USE$2,056,771
· FY2015 · Assistant Secretary for Fossil Energy
TAS::89 0222::TAS NEW PHASE I 2010 STTR; TITLE: ADVANCED METHODS FOR PREDICTING 3D UNSTEADY FLOWS AROUND WIND TURBINE BLADES; PI: GLEN WHITEHOUSE$1,307,526
· FY2010 · Department of Energy
REVISITING PIPE COMPONENT DESIGN$1,299,166
· FY2019 · Department of Energy
DISTRIBUTED LOW POWER ON-BLADE CONTROL FOR WIND TURBINE LOAD MITIGATION$980,589
· FY2015 · Department of Energy
BUBBLE THERMOGRAPHY VELOCIMETRY FOR URBAN FLOW FIELD CHARACTERIZATION$249,269
· FY2025 · Department of Energy
HIGH PERFORMANCE COLD SPRAY NOZZLE DESIGN USING COMPRESSED AIR FOR REPAIR OF NUCLEAR COMPONENTS$206,300
· FY2025 · Department of Energy
DEVELOPMENT OF A MODULAR MULTIPHYSICS SIMULATION PLATFORM FOR AEROSOL AND PARTICULATE DISPERSION MODELING$205,755
· FY2025 · Department of Energy
DEVELOPMENT OF HIGH-FIDELITY, MACHINE-LEARNING COMPATIBLE COMPUTATIONAL FLUID DYNAMICS SOFTWARE MODULES BASED ON AMREX$205,499
· FY2025 · Department of Energy
DESIGN SUPPORT METHODOLOGIES AND TOOL-CHAIN FOR HYDROGEN FUEL CELL REGIONAL AND URBAN AIR MOBILITY AIRCRAFT$199,752
· FY2023 · Department of Energy
NEW CLASSES OF AIRCRAFT PROVIDING PERSONAL ON-DEMAND MOBILITY ARE UNDER DEVELOPMENT AND ARE POISED TO REVOLUTIONIZE SHORTDURATION AIR TRAVEL. THE IMPETUS FOR THIS WORK COMES FROM ADVANCES IN ELECTRONICS AND CONTROLS AND INCREASES IN ELECTRIC MOTOR POWER DENSITIES. AS THESE AIRCRAFT ARE INTEGRATED INTO THE TRANSPORTATION SYSTEM THEY WILL ENCOUNTER ICING CONDITIONS THAT MAY CHALLENGE THE DESIGN PERFORMANCE OF THESE VEHICLES. THIS EFFORT WILL MAP A PATENTED ALGORITHMIC ICING DETECTION SCHEME PREVIOUSLY DEVELOPED FOR USE ON THE NAVY S V-22 OSPREY TILTROTOR TO THE PROPELLER/ROTOR SYSTEMS FOR THIS CATEGORY OF AIR VEHICLE WITH EXTENSIONS FOR USING MEASUREMENTS ON THE ELECTRIC MOTOR ITSELF TO INFER BOTH ICING LEVEL AND ICING GROWTH DURING FLIGHT OPERATIONS. BY FOCUSING THE DETECTION FILTER TO THE LIFT/PROPULSION SUBSYSTEM THE DETECTION ALGORITHM MAY BE HOSTED DIRECTLY WITHIN THE MOTOR CONTROL PROCESSOR ELECTRONICS THUS ALLOWING FOR DISTRIBUTED ICING SENSING CONCOMITANT WITH SUCH VEHICLE S DISTRIBUTED PROPULSION CONFIGURATIONS. AS THESE VTOL VEHICLES ARE DOMINATED BY LIFTING PROPELLER/ROTORS THE DETERMINATION OF THE LEVEL OF ICING ON THIS IMPORTANT COMPONENT FOR THESE AIRCRAFT WILL ENHANCE SAFETY AND MAY BE USED FOR ICING MITIGATION AND/OR VEHICLE FLIGHT GUIDANCE. THE PROPOSED WORKPLAN INCLUDES A TEST DEMONSTRATION OF THE TECHNOLOGY ON A REPRESENTATIVE LIFT/PROPULSION SUBSYSTEM USING SIMULATED ICING SHAPES ON THE LIFTING SURFACES.$8,364
· FY2020 · National Aeronautics and Space Administration