SBIR/STTR Research Award

SHEAR STRESS SENSOR DEVELOPMENT USING SURFACE ACOUSTIC WAVES

Award identifier 670d8a08ec6720c193415cb823c1a0c73aee5dcadf6f7a98fb8e49e769e6f2f6Awarding agency National Aeronautics and Space Administration

Award amount

$220,550

Program and phase

SBIR · Phase II

Award year

1986

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Raman Aeronautics Inc.
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

THIS PROJECT CONCERNS THE DEVELOPMENT OF A SMALL, RELIABLE AND UNIVERSALLY ACCEPTABLE SURFACE SHEAR STRESS (OR SKIN FRICTION) SENSOR FOR AERODYNAMIC BOUNDARY LAYER RESEARCH AT SUBSONIC TO SUPERSONIC SPEED. FOR THIS EFFORT THE SURFACE ACOUSTIC WAVE (SAW) DELAY-LINE TECHNIQUE (PHASE I) AND RESONATOR TECHNIQUE (PHASE II) WILL BE EXPLORED. DEPOSITION OF INTERDIGITAL TRANSDUCERS AND BENCH TESTING (PHASE I) AND DESIGN OF PROPER ENCLOSURE FOR THE SAW ELEMENT AND WIND TUNNEL TESTING (PHASE II) ARE PLANNED.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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