{"copyright":{"thirdPartyPermissionsProduced":false,"disclosedToPublic":false,"containsIndication":false,"publisherPermissionOrRightsToDistribute":false,"belongsToUsGov":false,"determinationType":"GOV_PUBLIC_USE_PERMITTED","thirdPartyContentCondition":"NOT_SET","belongsToContractor":false,"disclosedInvention":false,"submissionId":19930093029,"containsThirdPartyMaterial":false,"belongsToPublisher":false,"id":"8832bee279824bd4b9d9030e49d6bc2d","belongsToAuthors":false},"subjectCategories":["Aerodynamics"],"keywords":["TANK TESTS (NACA-#1)","TAKE-OFF - SEAPLANES - KAISER-HUGHES","SEAPLANES, CARGO","SEAPLANES - KAISER-HUGHES ( NACA 183) - RESISTANCE (AMER )"],"exportControl":{"isExportControl":"NO","submissionId":19930093029,"ear":"NO","id":"ed7bcde21ad849daaae5215f6d9fac26","itar":"NO"},"distributionDate":"2019-06-26T00:00:00.0000000+00:00","otherReportNumbers":["NACA-WR-L-683","Report Number: NACA-WR-L-683"],"title":"Resistance Tests of a 1/16 Size Model of the Hughes-kaiser Flying Boat, NACA Model 183","stiType":"OTHER","distribution":"PUBLIC","submittedDate":"2013-09-06T18:31:00.0000000+00:00","authorAffiliations":[{"sequence":0,"submissionId":19930093029,"meta":{"author":{"name":"Posner, Jack"},"organization":{"name":"National Advisory Committee for Aeronautics. Langley Aeronautical Lab.","location":"Langley Field, VA, United States"}},"id":"b19fa2cb8a834a5683bb296881e2b058"},{"sequence":1,"submissionId":19930093029,"meta":{"author":{"name":"Woodward, David R."},"organization":{"name":"National Advisory Committee for Aeronautics. Langley Aeronautical Lab.","location":"Langley Field, VA, United States"}},"id":"9d2918abd9f74965879e5e6fbaeb4238"},{"sequence":2,"submissionId":19930093029,"meta":{"author":{"name":"Olson, Roland E."},"organization":{"name":"National Advisory Committee for Aeronautics. Langley Aeronautical Lab.","location":"Langley Field, VA, United States"}},"id":"062675b7990049b88a8daa32793650c2"}],"stiTypeDetails":"Other - NACA Wartime Report","technicalReviewType":"TECHNICAL_REVIEW_TYPE_NONE","modified":"2025-08-31T18:39:21.7150190+00:00","id":19930093029,"sourceIdentifiers":[{"number":"hdl:100.2/ADA800650","submissionId":19930093029,"id":"ee9bb45c88ac44e186824ddc93a28c8d","type":"HANDLE"},{"submissionId":19930093029,"id":"ba8a2361dad146779e9aaaf9a98569af","descriptor":"hdl:100.2/ADA800650"}],"legacyMeta":{"__type":"LegacyMetaIndex, StrivesApi.ServiceModel","accessionNumber":"93R22319"},"created":"2013-09-06T18:31:00.0000000+00:00","center":{"code":"CDMS","name":"Legacy CDMS","id":"092d6e0881874968859b972d39a888dc"},"onlyAbstract":false,"sensitiveInformation":2,"abstract":"Tank tests were made of a hull model of the Hughes-Kaiser cargo airplane for estimates of take-off performance and maximum gross load for take-off. At hump speeds, with the model free to trim, the trim and resistance were high, which resulted in a load-resistance ratio of approximately 4.0 for a gross load coefficient of 0.75. With a 4000,000-lb load, the full size craft may take off in 69 sec over a distance of 5600 ft.","isLessonsLearned":false,"disseminated":"DOCUMENT_AND_METADATA","publications":[{"submissionId":19930093029,"id":"7d8e5a3f43fc4e1d996dff16b4083c71","publicationDate":"1944-06-01T00:00:00.0000000+00:00"}],"status":"CURATED","related":[],"downloads":[{"draft":false,"mimetype":"application/pdf","name":"19930093029.pdf","type":"STI","links":{"original":"/api/citations/19930093029/downloads/19930093029.pdf","pdf":"/api/citations/19930093029/downloads/19930093029.pdf","fulltext":"/api/citations/19930093029/downloads/19930093029.txt"}}],"downloadsAvailable":true,"index":"submissions-2026-05-07-04-55"}