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ACTIVE NOISE CONTROL FAN STATOR BLADE HOLOGRAPHY TEST

ACTIVE NOISE CONTROL FAN STATOR BLADE HOLOGRAPHY TEST

ACTIVE NOISE CONTROL FAN STATOR BLADE HOLOGRAPHY TEST

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NASA ACTIVE NOISE CONTROL FAN - Glenn Research Center History

BUNSEN BURNER TEST OF GRAPHITE FIBER FOLYIMIDE COMPOSITES

WINDMILL ROTOR BLADE FOR STATIC BLADE TEST

WINDMILL ROTOR BLADE FOR STATIC BLADE TEST

WINDMILL ROTOR BLADE FOR STATIC BLADE TEST

ACTIVE NOISE CONTROL FAN STATOR BLADE HOLOGRAPHY TEST

description

Summary

ACTIVE NOISE CONTROL FAN STATOR BLADE HOLOGRAPHY TEST

NASA Identifier: GRC-C-1996-3562

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Tags

nasa active noise control fan stator blade holography test dvids high resolution glenn research center aviation research organization
date_range

Date

1996
place

Location

create

Source

Defense Visual Information Distribution Service
link

Link

https://www.dvidshub.net/
copyright

Copyright info

Public Domain Dedication. Public Use Notice of Limitations: https://www.dvidshub.net/about/copyright

label_outline Explore Dvids, Aviation Research Organization, Glenn Research Center

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Orion Capsule and Launch Abort System (LAS) installed in the NASA Glenn 8x6 Supersonic Wind Tunnel (SWT) for testing. This test is an Aero Acoustic test of the LAS

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nasa active noise control fan stator blade holography test dvids high resolution glenn research center aviation research organization