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Company Information:

Name: High Technology Corporation
Address: 28 Research Drive
Hampton, VA 23666
Located in HUBZone: No
Woman-Owned: No
Minority-Owned: Yes
URL: N/A
Phone: (757) 865-0818

Award Totals:

Program/Phase Award Amount ($) Number of Awards
SBIR Phase I $1,756,016.00 27
SBIR Phase II $5,688,627.00 10
STTR Phase I $100,000.00 1

Award List:

STABILITY AND TRANSITION IN CHEMICALLY REACTING NONEQUILIBRIUM FLOWS

Award Year / Program / Phase: 1988 / SBIR / Phase I
Agency / Branch: DOD / DARPA
Principal Investigator: Dr mujeeb r malik
Award Amount: $50,608.00
Abstract:
It is proposed here to develop a method for prediction of transition on nasp (national aero-space plane) configuration and for the control/enhancement of supersonic combustion in the scramjet. the method is based upon linear stability analysis with noneequilibrium effects which typify the boundary… More

NUMERICAL AND ANALYTIAL STUDIES OF LAMINAR TO TURBULENCE TRANSITION

Award Year / Program / Phase: 1989 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Dr Mujeeb R Malik
Award Amount: $49,920.00

NUMERICAL AND ANALYTIAL STUDIES OF LAMINAR TO TURBULENCE TRANSITION

Award Year / Program / Phase: 1990 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Dr Mujeeb R Malik
Award Amount: $179,309.00
Abstract:
It is proposed here to study nonlinear development of gortler and crossflow vortices and investigate various wave-interaction mechanisms operative in two and three-dimensional boundary layers. the proposed work will numerically simulate transition in a threedimensional boundary layer. the objective… More

ADVANCED COMPUTATIONAL TECHNIQUES IN STUDIES OF HYPERSONIC BOUNDARY-LAYER TRANSITION

Award Year / Program / Phase: 1990 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Mujeeb R Malik
Award Amount: $49,994.00
Abstract:
The objective of the proposed work is to use advanced theoretical and computational techniques for studies of hypersonic boundary layer stability and transition to turbulence. these studies will enhance our understanding of the transition phenomena and thus help predict and control transition with a… More

Transition Prediction and Laminar Flow Control in Compressible 3D Boundary Layers Using PSE

Award Year / Program / Phase: 1993 / SBIR / Phase I
Agency: NASA
Principal Investigator: Mujeeb R. Malik
Award Amount: $49,927.00

Transistion Control in Corner Flow of a Supersonic Square Nozzle

Award Year / Program / Phase: 1994 / SBIR / Phase I
Agency: NASA
Principal Investigator: Ray-Sing Lin
Award Amount: $67,548.00
Abstract:
"Quiet" (low-disturbance) wind tunnels, needed for transitionresearch, require cleverly designed nozzle contours forstabilization or delay of dominant instabilities in supersonicnozzle wall boundary layers. However, if a nozzle of squarecross-section

Drag-Prediction Algorithms for Navier-Stokes Solutions over Single- and Multi-Element Airfoils

Award Year / Program / Phase: 1994 / SBIR / Phase I
Agency: NASA
Principal Investigator: Paul M. Vijgen
Award Amount: $68,760.00
Abstract:
Accurate prediction of the aerodynamic lift and drag is acritical requirement in the development process of an aircraft.Presently, computational methods based on numerical solution ofthe Reynolds-averaged Navier-Stokes (N-S) equations are beingapplie

Active Suppression of Resonance Interactions between Shear-Layers and Cavities

Award Year / Program / Phase: 1994 / SBIR / Phase I
Agency: NASA
Principal Investigator: Richard W. Wlezien
Award Amount: $68,801.00

Supersonic Jet-Noise Prediction and Control

Award Year / Program / Phase: 1994 / SBIR / Phase I
Agency: NASA
Principal Investigator: Ponnampalam Balakumar
Award Amount: $68,458.00

Transition Prediction and Laminar Flow Control in Compressible 3D Boundary Layers Using PSE

Award Year / Program / Phase: 1994 / SBIR / Phase II
Agency: NASA
Principal Investigator: Mujeeb R. Malik
Award Amount: $485,880.00

Active Suppression of Resonance Interactions between Shear-Layers and Cavities

Award Year / Program / Phase: 1995 / SBIR / Phase II
Agency: NASA
Principal Investigator: Richard W. Wlezien
Award Amount: $599,767.00
Abstract:
The control of the resonant interaction between a free shearlayer and an open cavity is of direct relevance to wind-tunneltesting and aircraft applications. Techniques will beinvestigated for the control of acoustic resonances in opencavity flows. Th

Supersonic Jet-Noise Prediction and Control

Award Year / Program / Phase: 1995 / SBIR / Phase II
Agency: NASA
Principal Investigator: Ponnampalam Balakumar
Award Amount: $598,302.00
Abstract:
Recent studies have demonstrated that a definite relation existsbetween instability waves and noise of high-speed jets and,hence, the instability wave model can be used to predict certainfeatures of the jet noise. The instability model used in theses

Optimization Of Suction For Laminar Flow Control Applications

Award Year / Program / Phase: 1995 / SBIR / Phase I
Agency: NASA
Principal Investigator: Jamal A. Masad , Research Scientist
Award Amount: $67,822.00

Prediction and Active Control of Flow-Induced Weapons Bay Acoustics

Award Year / Program / Phase: 1995 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Louis N. Cattafesta, Iii
Award Amount: $79,653.00

Active Control/Alleviation Of Trailing (Streamwise) Vortices

Award Year / Program / Phase: 1995 / SBIR / Phase I
Agency: NASA
Principal Investigator: Mehdi R. Khorrami , Research Scientist
Award Amount: $68,821.00

Prediction and Active Control of Flow-Induced Weapons Bay Acoustics

Award Year / Program / Phase: 1996 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Louis N. Cattafesta, Iii
Award Amount: $737,215.00
Abstract:
The modeling and active control of the resonant interaction between a free shear layer and an open cavity is of direct relevance to military aircraft applications. Techniques will be investigated to first model and then control acoustic resonance in open cavity flows. The problem consists of the… More

HYBRID LAMINAR FLOW CONTROL TECHNIQUE FOR ENGINE NACELLES

Award Year / Program / Phase: 1996 / SBIR / Phase I
Agency: NASA
Principal Investigator: Jamal A. Masad , Research Scientist
Award Amount: $69,910.00

A PROGRAMMING ENVIRONMENT FOR THE DEVELOPMENT OF LARGE SCIENTIFIC SYSTEMS ON A DISTRIBUTED COMPUTING NETWORK

Award Year / Program / Phase: 1996 / SBIR / Phase I
Agency: NASA
Principal Investigator: Thomas M. Eidson , Senior Scientist
Award Amount: $69,894.00

Optimization Of Suction For Laminar Flow Control Applications

Award Year / Program / Phase: 1996 / SBIR / Phase II
Agency: NASA
Principal Investigator: Jamal A. Masad , Research Scientist
Award Amount: $587,826.00

LAMINAR-TURBULENT TRANSITION PREDICTION OF REACTING FLOWS IN HYPERSONIC VEHICLES APPLICATION

Award Year / Program / Phase: 1996 / SBIR / Phase I
Agency: NASA
Principal Investigator: Chau-lyan Chang , Research Scientist
Award Amount: $68,868.00

A Novel Computational Tool For Hypersonic Transition Prediction

Award Year / Program / Phase: 1997 / SBIR / Phase I
Agency: NASA
Principal Investigator: Mujeeb R. Malik , CHIEF SCIENTIST
Award Amount: $67,032.00

A PROGRAMMING ENVIRONMENT FOR THE DEVELOPMENT OF LARGE SCIENTIFIC SYSTEMS ON A DISTRIBUTED COMPUTING NETWORK

Award Year / Program / Phase: 1997 / SBIR / Phase II
Agency: NASA
Principal Investigator: Thomas M. Eidson , Senior Scientist
Award Amount: $570,483.00

LAMINAR-TURBULENT TRANSITION PREDICTION OF REACTING FLOWS IN HYPERSONIC VEHICLES APPLICATION

Award Year / Program / Phase: 1997 / SBIR / Phase II
Agency: NASA
Principal Investigator: Chau-lyan Chang , Research Scientist
Award Amount: $580,103.00

Advanced Actuator Systems for Separation Control

Award Year / Program / Phase: 1998 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Louis N. Cattafesta, Iii
Award Amount: $100,000.00
Abstract:
The development of actuators suitable for boundary-layer separation control is proposed. The Phase I effort focuses on the analysis, design, fabrication, and benchtop testing of prototype systems. The actuators will generate disturbances that are large enough to significantly influence the… More

A Novel Computational Tool for Transition Prediction over Hypersonic Vehicles

Award Year / Program / Phase: 1998 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Mujeeb R. Malik
Award Amount: $100,000.00
Abstract:
Laminar to turbulent transition phenomenon in hypersonic flows remains poorly understood although it has a profound impact on the thermal protection system weight, vehicle drag and air-breathing engine performance. Transition location uncertainty forces designers to be conservative by adding weight… More

Advanced Prediction Tool for Simulation of Turbomachinery Noise Sources

Award Year / Program / Phase: 1998 / SBIR / Phase I
Agency: NASA
Principal Investigator:
Award Amount: $70,000.00

An advanced system for dynamic model deformation and angle-of-attack measurements

Award Year / Program / Phase: 1998 / SBIR / Phase I
Agency: NASA
Principal Investigator:
Award Amount: $70,000.00

Control and Alteration of Wing-Tip Flowfield for Induced Drag Reduction

Award Year / Program / Phase: 1998 / SBIR / Phase I
Agency: NASA
Principal Investigator:
Award Amount: $70,000.00

A Novel Approach for Mitigation of Rotor Tip-Clearance Induced noise in Turbofan Engines

Award Year / Program / Phase: 1999 / SBIR / Phase I
Agency: NASA
Principal Investigator: Mehdi R. Khorrami, Senior Scientist
Award Amount: $70,000.00

High-Lift Transition Prediction Module

Award Year / Program / Phase: 1999 / SBIR / Phase I
Agency: NASA
Principal Investigator: Ray-Sing Lin, Research Scientist
Award Amount: $70,000.00

A Lifetime Pressure Sensitive Paint (PSP) and Model Deformation Imaging System

Award Year / Program / Phase: 1999 / SBIR / Phase I
Agency: NASA
Principal Investigator: Louis N. Cattafesta III, Senior Research Scientist
Award Amount: $70,000.00

N/A

Award Year / Program / Phase: 2000 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Mujeeb R. Malik, Chief Scientist
Award Amount: $100,000.00

A Photogrammetric Imaging System for Measurement of Flight Control Surfaces

Award Year / Program / Phase: 2001 / SBIR / Phase I
Agency: NASA
Principal Investigator: Deepak Shukla, Research Scientist
Award Amount: $70,000.00
Abstract:
The development of a commercially viable photogrammetric system is proposed for measurement of motion and deformation of flight control surfaces. This system will measure the position, velocity and deformation of flight control surfaces in an aircraft where such deformation typically includes… More

USAT: Unified Software for Analysis of Transition

Award Year / Program / Phase: 2002 / SBIR / Phase II
Agency / Branch: DOD / USAF
Principal Investigator: Mujeeb R. Malik, Chief Scientist
Award Amount: $759,742.00
Abstract:
"Laminar-Turbulent transition phenomenon in hypersonic flows remains poorly understood although it has a profound impact on the thermal protection system weight, vehicle drag and air-breathing engine performance. Transition location uncertainties forcedesigners to be conservative by adding weight… More

A Real-Time Photogrammetric Imaging System for Flight Control Surfaces

Award Year / Program / Phase: 2002 / SBIR / Phase I
Agency: NASA
Principal Investigator: Deepak Shukla, Research Scientist
Award Amount: $0.00
Abstract:
The development of a commercially viable photogrammetric system is proposed for measurement of motion and deformation of flight control surfaces. This system will measure the position, velocity and deformation of flight control surfaces in an aircraft where such deformation typically includes… More

A Real-Time Photogrammetric Imaging System for Flight Control Surfaces

Award Year / Program / Phase: 2002 / SBIR / Phase II
Agency: NASA
Principal Investigator: Deepak Shukla, Research Scientist
Award Amount: $590,000.00
Abstract:
The development of a commercially viable photogrammetric system is proposed for measurement of motion and deformation of flight control surfaces. This system will measure the position, velocity and deformation of flight control surfaces in an aircraft where such deformation typically includes… More

USAT: Unified Software for Analysis of Transition

Award Year / Program / Phase: 2002 / SBIR / Phase I
Agency / Branch: DOD / USAF
Principal Investigator: Mujeeb R. Malik, Chief Scientist
Award Amount: $0.00
Abstract:
"Laminar-Turbulent transition phenomenon in hypersonic flows remains poorly understood although it has a profound impact on the thermal protection system weight, vehicle drag and air-breathing engine performance. Transition location uncertainties forcedesigners to be conservative by adding weight… More