{"copyright":{"thirdPartyPermissionsProduced":false,"disclosedToPublic":false,"containsIndication":false,"publisherPermissionOrRightsToDistribute":false,"belongsToUsGov":false,"determinationType":"GOV_PUBLIC_USE_PERMITTED","thirdPartyContentCondition":"NOT_SET","belongsToContractor":false,"disclosedInvention":false,"submissionId":19800007942,"containsThirdPartyMaterial":false,"belongsToPublisher":false,"id":"c7358da6cc1449df8560117031fc786b","belongsToAuthors":false},"subjectCategories":["Aircraft Design, Testing And Performance"],"exportControl":{"isExportControl":"NO","submissionId":19800007942,"ear":"NO","id":"3e9342fd4d1e4abfb1f55b7081b4303f","itar":"NO"},"distributionDate":"2011-09-08T00:00:00.0000000+00:00","title":"Status of cavity noise phenomena measurement and suppression on the B-1 aircraft","stiType":"CONFERENCE_PAPER","distribution":"PUBLIC","submittedDate":"2013-08-10T13:56:00.0000000+00:00","authorAffiliations":[{"sequence":0,"submissionId":19800007942,"meta":{"author":{"name":"Tipton, A. G."},"organization":{"name":"Rockwell International Corp.","location":"El Segundo, CA, United States"}},"id":"bb2653f3de214f5d83599d813470b41c"},{"sequence":1,"submissionId":19800007942,"meta":{"author":{"name":"Hodson, C. H."},"organization":{"name":"Rockwell International Corp.","location":"El Segundo, CA, United States"}},"id":"6c2129f9470545feadc48c673f8913dd"}],"stiTypeDetails":"Conference Paper","technicalReviewType":"TECHNICAL_REVIEW_TYPE_NONE","modified":"2025-08-31T18:39:21.7150190+00:00","id":19800007942,"legacyMeta":{"__type":"LegacyMetaIndex, StrivesApi.ServiceModel","accessionNumber":"80N16202"},"created":"2013-08-10T13:56:00.0000000+00:00","center":{"code":"CDMS","name":"Legacy CDMS","id":"092d6e0881874968859b972d39a888dc"},"onlyAbstract":false,"sensitiveInformation":2,"abstract":"During the B-1 aircraft development, an extensive program of weapons bay cavity noise measurement and suppression studies was performed using wind tunnel models, flight test measurements, and aircraft design modifications. Substantial cavity noise reduction was demonstrated during flight test operations. The unsuppressed cavity noise level of 170 dB was reduced to values less than 150 dB with external retractable spoilers upstream of the cavity opening.","isLessonsLearned":false,"disseminated":"METADATA_ONLY","publications":[{"submissionId":19800007942,"id":"5d31f03f50c148d38ed46f2d7d1c5a82","publicationName":"Shock and Vibration Inform. Center  The Shock and Vibration Bull., Pt 1","publicationDate":"1979-09-01T00:00:00.0000000+00:00"}],"status":"CURATED","related":[{"disseminated":"DOCUMENT_AND_METADATA","id":19800007938,"type":"ANALYTIC_PRIMARY","title":"The Shock and Vibration Bulletin. Part 1: Invited Papers, Vibrations and Acoustics, Blast and Shock","stiType":"CONFERENCE_PROCEEDINGS","distribution":"PUBLIC","accessionNumber":"N80-16199 through N80-16210","status":"CURATED"},{"disseminated":"DOCUMENT_AND_METADATA","id":19800007938,"type":"ANALYTIC_PRIMARY","title":"The Shock and Vibration Bulletin. Part 1: Invited Papers, Vibrations and Acoustics, Blast and Shock","stiType":"CONFERENCE_PROCEEDINGS","distribution":"PUBLIC","status":"CURATED"}],"downloads":[],"downloadsAvailable":true,"index":"submissions-2026-10-15-05-24"}