Structural Integrity Assoc., Inc.

3150 Almaden Expressway Suite 145
San Jose, CA 95118
50 Employees

SBIR Award Summary

Total Number of Awards 8
Total Value of Awards $1.85MM
First Award Date 01/01/86
Most Recent Award Date 05/23/95

Key Personnel

Last Name Name Awards Contact
Kuo Dr. An-Yu Kuo 4
Tang Shu Tang 1
Kuo An-Yu Kuo 1
Tang Shu Tang 1
LICINA George J LICINA 1

8 Awards Won

Phase 2 SBIR

Agency: Air Force
Topic: AF94-170
Budget: 05/23/95 - 05/23/97

Feasibility of developing an expert design system for plastic IC packages against moisture-induced defects has been demonstrated in the Phase I study. It is proposed that an expert design system wit a material properties database, tools for computer simulation, and design rules be integrated. Existing mechanical properties of all common materia...

Phase 1 SBIR

Agency: Air Force
Topic: AF94-170
Budget: 05/24/94 - 11/24/94

A feasibility study of developing an expert design system for plastic integrated circuit packages against latent moisture-induced defects is proposed. Moisture-induced cracking of the package is one common type of latent defect incurred during board assembly. Heat transfer, moisture diffusion, moisture vaporization, thermal stress, hydro stress...

Phase 1 SBIR

Agency: Navy
Topic: N93-100
Budget: 01/12/93 - 01/15/94

Phase 2 SBIR

Agency: Army
Topic: A89-004
Budget: 12/23/91 - 06/23/93
PI: Shu Tang

A methodology for on-line fatigue monitoring of non-airframes components of rotorcraft has been developed under Phase I of this project. It is a semi-empirical method, using a combination of pattern recognition, load-cycle spectrum classification, an correlated load ranges. It was demonstrated to efficiently predict the fatigue usage of a rota...

Phase 1 SBIR

Agency: Army
Topic: A89-004
Budget: 09/28/89 - 12/31/89
PI: Shu Tang

Phase 1 SBIR

Agency: Air Force
Topic: AF89-114
Budget: 01/01/89 - 12/31/89
PI: An-Yu Kuo

Phase 2 SBIR

Agency: Air Force
Topic: AF86-136
Budget: 01/01/87 - 12/31/87

UNDER PHASE I OF THIS STUDY, A NOVEL METHOD WAS DEVELOPED AND DEMONSTRATED FOR CALCULATING CRACKTIP STRESS INTENSITY FACTORS FOR CRACKED METAL STRUCTURES UNDER RAPID THERMAL PULSE LOADINGS. THE METHOD COUPLES A GREEN'S FUNCTION INTEGRATION TECHNIQUE FOR TRANSIENT THERMAL STRESSES WITH THE WELL-KNOWN INFLUENCE FUNCTION APPROACH FOR CALCULATING S...

Phase 1 SBIR

Agency: Air Force
Topic: AF86-136
Budget: 01/01/86 - 12/31/86