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Company Information:

Company Name: CMSoft, Inc.
City: Palo Alto
State: CA
Zip+4: 94306
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
Phone: (650) 353-0540

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $749,210.00 7
SBIR Phase II $3,576,249.00 6
STTR Phase I $79,962.00 1

Award List:

Buffet and Dynamic Loads Analysis

Award Year / Program / Phase: 2005 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Thuan Lieu, Research Scientist
Award Amount: $99,396.00
Abstract:
CFD (Computational Fluid Dynamics)-based nonlinear computational aeroelasticity methods have been successfully demonstrated for the flutter analysis of complete aircraft configurations in subsonic, transonic, and supersonic airstreams, at low to moderate angles of attack, for clean wing… More

Buffet and Dynamic Loads Analysis

Award Year / Program / Phase: 2006 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Thuan Lieu, Research Scientist
Award Amount: $721,968.00
Abstract:
CFD (Computational Fluid Dynamics)-based nonlinear computational aeroelasticity methods have been successfully demonstrated for the flutter analysis of complete aircraft configurations in subsonic, transonic, and supersonic airstreams, at low to moderate angles of attack, for clean wing… More

Ground Loads Predictive Analysis

Award Year / Program / Phase: 2006 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Thuan Lieu, Research Scientist
Award Amount: $99,998.00
Abstract:
The use of a reliable analysis tool for predicting aircraft ground loads during high-speed taxi can expedite ground loads testing during the certification of military aircraft. Therefore, the ultimate objective of this proposal is to develop GLAT, a state-of-the-art simulation tool for ground load… More

Aerothermoelastic Simulation

Award Year / Program / Phase: 2008 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Goeric Daeninck, Research Scientist
Award Amount: $99,965.00
Abstract:
Hypersonic flight introduces extreme heat loads into the skin of a vehicle, particularly at its leading edges. Determining these loads is a challenging task that requires accounting for the aerothermal features of both the flow and thermal state of the surface of the structure. Hence, the accurate… More

Geometric Proximity of Independent Systems Simulation

Award Year / Program / Phase: 2009 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Thuan Lieu, Research Scientist
Award Amount: $99,970.00
Abstract:
The pressing need for high-fidelity transient, nonlinear, viscous, fluid-structure simulations arises in the solution of many important engineering problems. These include not only the design of high-performance aircraft where flutter, limit cycle oscillation, and buffeting remain the most important… More

Systems Deployment & Relative Motion Analysis

Award Year / Program / Phase: 2009 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Thuan Lieu, Research Scientist
Award Amount: $99,987.00
Abstract:
Today, a pressing need for high-fidelity transient, nonlinear, viscous, multidisciplinary simulations of complex fluid-structure systems with associated subsystems operating in near space arises in the design and analysis of many engineering operations. These include not only the cargo/weapon… More

Aeroacoustic Analysis

Award Year / Program / Phase: 2009 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Goerick Daeninck, Research Scientist
Award Amount: $99,982.00
Abstract:
The reduction of aerodynamic/hydrodynamic noise caused by violent turbulence is of strategic importance to many military systems. These include modern fighter aircraft, unmanned weapons with sensitive electronics, and underwater vehicles. For all these systems, aerodynamic or hydrodynamic noise can… More

Aerothermoelastic Simulation

Award Year / Program / Phase: 2009 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Goeric Daeninck, Research Scientist
Award Amount: $586,279.00
Abstract:
Testing and clearing hypersonic systems is a challenging task. When anything unexpected occurs, the time to react is so short that the tested article must be destroyed. Because ground-based experimental facilities such as shock tunnels and arc-jets are typically unable to reproduce the flight… More

Geometric Proximity of Independent Systems Simulation

Award Year / Program / Phase: 2010 / SBIR / Phase II
Agency: DOD
Principal Investigator: Thuan Lieu, Research Scientist – (650) 855-9310
Award Amount: $584,016.00
Abstract:
The pressing need for high-fidelity transient, nonlinear, viscous, fluid-structure simulations arises in the solution of many important engineering problems. These include not only the design of high-performance aircraft where flutter, limit cycle oscillation, and buffeting remain the most important… More

Systems Deployment&Relative Motion Analysis

Award Year / Program / Phase: 2011 / SBIR / Phase II
Agency: DOD
Principal Investigator: Thuan Lieu, Research Scientist – (650) 855-9310
Award Amount: $594,642.00
Abstract:
ABSTRACT: Today, a pressing need for high-fidelity transient, nonlinear, viscous, multidisciplinary simulations of complex fluid-structure systems with associated subsystems operating in near space arises in the design and analysis of many engineering operations. These include not only the… More

Aeroacoustic Analysis

Award Year / Program / Phase: 2011 / SBIR / Phase II
Agency: DOD
Principal Investigator: Goeric Daeninck, Research Scientist – (650) 855-9310
Award Amount: $594,474.00
Abstract:
ABSTRACT: The reduction of aerodynamic/hydrodynamic noise caused by violent turbulence is of strategic importance to many military systems. These include modern fighter jets, unmanned weapons with sensitive electronics, and surface and underwater vessels. For all these systems, aerodynamic or… More

Increased Capability and Interface for Computational Code for Implosion

Award Year / Program / Phase: 2012 / SBIR / Phase I
Agency / Branch: DOD / NAVY
Principal Investigator: Goeric Daeninck, Research Scientist – (650) 855-9310
Award Amount: $149,912.00
Abstract:
This SBIR Phase I project aims at enabling the transformation of the computational capability for implosion developed under the ONR MURI and FNC programs on implosion from a research code to a reliable, high-performance, and user-friendly software for the prediction of implosion and its effects on… More

High Efficiency Computation of High Reynolds Number Flows via Anisotropic Adaptive Mesh Refinement

Award Year / Program / Phase: 2013 / STTR / Phase I
Agency / Branch: DOD / NAVY
Research Institution: University of Washington
Principal Investigator: Goeric Daeninck, Research Scientist – (650) 614-1101
Award Amount: $79,962.00
RI Contact: Ulrich Hetmaniuk
Abstract:
This STTR Phase I project aims to design, implement, and demonstrate a rigorous, practical, fast, and re-usable anisotropic mesh adaptation software module for enabling the efficient computation of high Reynolds number flows in large computational domains. To this effect, it focuses on developing:… More

Increased Capability and Interface for Computational Code for Implosion

Award Year / Program / Phase: 2013 / SBIR / Phase II
Agency: DOD
Principal Investigator: Arthur Rallu, Research Scientist – (650) 855-9310
Award Amount: $494,870.00
Abstract:
This SBIR Phase II project will transform the computational capability for implosion developed under the ONR MURI and FNC programs on implosion from a research code to a reliable, high-performance, and user-friendly software for the prediction of underwater implosion. To this effect, the finite… More