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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.

Download all SBIR.gov award data either with award abstracts (290MB) or without award abstracts (65MB). A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.

The SBIR.gov award data files now contain the required fields to calculate award timeliness for individual awards or for an agency or branch. Additional information on calculating award timeliness is available on the Data Resource Page.

Displaying 205251 - 205260 of 207712 results
  1. SPARSE LINEAR SYSTEMS OF EQUATIONS IN A VECTOR PROCESSING ENVIRONMENT

    SBC: Scientific Comput Assoc            Topic: N/A

    THIS PROJECT IS TO BUILD A VECTOR PROCESSING VERSION OF PCGPAK, THE PRECONDITIONED CONJUGATE GRADIENT PACKAGE OF SUBROUTINES FOR ITERATIVE SOLUTION OF LARGE, SPARSE, NONSYMMETRIC SYSTEMS OF LINEAR EQUATIONS. THE PCGPAK IS CURRENTLY BEING MARKETED AND IS THE RESULT OF INTERNAL DEVELOPMENT WORK IMPLEMENTING TECHNIQUES FOR ITERATIVE SOLUTION OF SPARSE SYSTEMS DEVELOPED BY RESEARCHERS IN ACADEMIA. PCG ...

    SBIR Phase I 1985 Department of Energy
  2. NONLINEAR SYSTEMS OF EQUATIONS

    SBC: Scientific Comput Assoc            Topic: N/A

    WE PROPOSE TO BUILD A STATE-OF-THE-ART SOFTWARE PACKAGE FOR SOLVING GENERAL LARGE SYSTEMS OF NONLINEAR EQUATIONS. ALTHOUGH THERE ARE SEVERAL SOFTWARE PACKAGES FOR SOLVING LARGE SPARSE LINEAR SYSTEMS (SPARSEPACK, YSMP, HAREWELL, FOR EXAMPLE), SIMILAR PACKAGES FOR NONLINEAR SYSTEMS ARE ALMOST NONEXISTENT. WE PROPOSE TO CONSTRUCT A COLLECTION OF ROUTINES INCORPORATING WELL-ESTABLISHED VARIATIONS OF N ...

    SBIR Phase I 1985 Department of DefenseAir Force
  3. MODIFICATION AND IMPROVEMENT OF SOFTWARE FOR MODELING MULTI DIMENSIONAL REACTION FUEL FLOW

    SBC: Scientific Comput Assoc            Topic: N/A

    N/A

    SBIR Phase I 1985 Department of DefenseAir Force
  4. A PROPOSAL FOR BUILDING AN INTERACTIVE SOFTWARE SYSTEM FOR SCIENTIFIC COMPUTATION ON SUPERCOMPUTERS

    SBC: Scientific Comput Assoc            Topic: N/A

    N/A

    SBIR Phase I 1985 National Science Foundation
  5. A PROPOSAL FOR BUILDING A LINDA COMPILER AND COMMUNICATION KERNEL FOR PARALLEL PROGRAMMING ON HYPERCUBE-CONNECTED MULTICOMPUTERS

    SBC: Scientific Comput Assoc            Topic: N/A

    N/A

    SBIR Phase I 1985 National Science Foundation
  6. NUMERICAL INVESTIGATION OF UNSTEADY THREE-DIMENSIONAL TURBULENT STRUCTDURES IN BOUNDARY LAYER FLOWS OVER AN AIRFOIL

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    A PROPOSAL IS PRESENTED HEREIN TO NUMERICALLY INVESTIGATE THE UNSTEADY DYNAMICS OF HAIRPIN VORTICS SUBMERGED IN VARIOUS BACKGROUND FLOWS. THE COMPUTER CODE TO BE USED WAS DEVELOPED FOR CALCULATING UNSTEADY THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER FLOWS ON WINGS AND IS CAPABLE OF TREATING NEGATIVE CROSS FLOW AND STREAMWISE REVERSE FLOW. UNDER PHASE I OF THE CURRENT PROPOSAL, THE BACKGROUND FLOW W ...

    SBIR Phase II 1985 Department of DefenseAir Force
  7. ADVANCED LABYRINTH SEALS

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    A PROPOSAL IS PRESENTED HEREIN TO EXTEND A RECENTLY DEVELOPED LABRYINTH SEAL ANALYSIS TO ENABLE IT TO BE APPLIED TO MORE ADVANCED SEALS WHICH HAVE RECENTLY BEEN PROPOSED FOR USE IN ADVANCED HIGH PERFORMANCE AXIAL TURBOMACHINERY. UNDER PHASE I OF THIS EFFORT, THE NECESSARY INITIAL COORDINATE SYSTEM DEVELOPMENT WILL BE UNDERTAKEN TO ENABLE THE CURVED SEAL LIPS CHARACTERISTICS OF THESE ADVANCED DESIG ...

    SBIR Phase II 1985 Department of DefenseAir Force
  8. AN INVESTIGATION IS PROPOSED HEREIN TO FORMALIZE, TEST AND EVALUATE NEW TECHNIQUES FOR IMPROVING THE TRANSIENT ACCURACYOF IMPLICIT FINITE-DIFFERENCE ALGORITHMS FOR THE TWO AND THREE-DIMENSIONAL COMPRESSIBLE NAVIER-STOKES EQUATIONS.

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    AN INVESTIGATION IS PROPOSED HEREIN TO FORMALIZE, TEST AND EVALUATE NEW TECHNIQUES FOR IMPROVING THE TRANSIENT ACCURACYOF IMPLICIT FINITE-DIFFERENCE ALGORITHMS FOR THE TWO AND THREE-DIMENSIONAL COMPRESSIBLE NAVIER-STOKES EQUATIONS. THEPROPOSED INVESTIGATION IS MOTIVATED BY THE NEED FOR COMPUTATIONAL METHODS OF IMPROVED ACCURACY AND EFFICIENCY FOR APPLICATION TO TRANSIENT MULTIDIMENSIONAL FLOWS IN ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  9. VISCOUS COMPUTATIONAL ANALYSIS AND A CONSTRAINED OPTIMIZATION TECHNIQUE

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    PROPER DUCT DESIGN IS A FUNDAMENTAL ENGINEERING PROBLEM WHICH CAN HAVE A MAJOR IMPACT UPON COMPNENT EFFICIENCY. CURRENT AEROSPACE APPLICATIONS, WHICH PLACE A PREMIUM ON COMPACT DESIGN AND CLOSELY FIT COMPONENTS, OFTEN EXACERBATE THIS PROBLEM. EXAMPLES ARE DUCTS ASSOCIATED WITH INLETS ANDNOZZLES AS WELL AS TRANSITION DUCTS BETWEEN ENGINE COMPONENTS. AT PRESENT TECHNOLOGY IS AVAILABLE TO COMPUTE THE ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
  10. A PROPOSAL IS PRESENTED HEREIN TO INITIATE A STUDY OF THE TRANSIENT BEHAVIOR OF A SILICON CHARGE COUPLED DEVICE (CCD) AND ITS RESPONSE TO INCIDENT RADIATION.

    SBC: SCIENTIFIC RESEARCH ASSOC., INC.            Topic: N/A

    A PROPOSAL IS PRESENTED HEREIN TO INITIATE A STUDY OF THE TRANSIENT BEHAVIOR OF A SILICON CHARGE COUPLED DEVICE (CCD) AND ITS RESPONSE TO INCIDENT RADIATION. THE MOTIVATION FOR THIS EFFORT IS BASED ON RECENT ANALYTICAL AND HARDWARE STUDIES WHICH HAVE IDENTIFIED THE POTENIALLY SIGNIFICANT BENEFITS I.E. REDUCED PSUEDONOISE (PN) CODE ACQUISITION TIME, THAT MAY BE ACHIEVED VIA THE APPLICATION OF CHARG ...

    SBIR Phase I 1985 National Aeronautics and Space Administration
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