LEADER 01938cam a2200505Ia 4500001 9972590723506421 005 20231120122710.0 007 cr c|||||||||| 008 121119s2012 ohua obt f000 0 eng d 035 ocn818645984 035 (NjP)7259072-princetondb 035 |z(NjP)Voyager7259072 040 GPO |beng |cGPO |dMvI 049 DOCS 074 0830-H-15 (online) 086 0 NAS 1.60:2012-215653 090 Electronic Resource 245 00 Assessment of NASA's aircraft noise prediction capability / |cMilo D. Dahl, editor. 264 1 Cleveland, Ohio : |bNational Aeronautics and Space Administration, Glenn Research Center, |c[2012] 300 1 online resource (xxxi, 354 pages) : |bcolor illustrations. 336 text |btxt |2rdacontent 337 computer |bc |2rdamedia 338 online resource |bcr |2rdacarrier 490 1 NASA/TP ; |v2012-215653 500 Title from title screen (viewed on Nov. 19, 2012). 500 "July 2012." 504 Includes bibliographical references. 536 Sponsored by National Aeronautics and Space Administration |hWBS 561581.02.08.03.18.03 536 |dE-15800 650 7 Aeroacoustics. |2nasat 650 7 Noise prediction (aircraft) |2nasat 650 7 Jet aircraft noise. |2nasat 650 7 Wind tunnel tests. |2nasat 650 7 Hypersonic aircraft. |2nasat 650 7 Subsonic aircraft. |2nasat 650 7 Rotary wing aircraft. |2nasat 650 7 Computational fluid dynamics. |2nasat 650 7 Aircraft noise. |2nasat 650 7 Supersonic aircraft. |2nasat 700 1 Dahl, Milo D., |d1956- 710 2 NASA Glenn Research Center. 776 08 |iPrint version: |tAssessment of NASA's aircraft noise prediction capability |w(OCoLC)823318882 830 0 NASA technical paper ; |v2012-215653. 945 DOCS |cNAS 1.60:2012-215653 956 40 |uhttps://purl.fdlp.gov/GPO/gpo31486