01691nam 2200505I 450 991070273460332120150203132632.0(CKB)5470000002430855(OCoLC)902680759(EXLCZ)99547000000243085520150203j201408 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierData reduction functions for the Langley 14- by 22-foot subsonic tunnel /Andy D. BoneyHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,August 2014.1 online resource (iii, 77 pages)NASA/TM ;2014-218513Title from title screen (viewed Feb. 3, 2015)."August 2014."Includes bibliographical references (page 77).Data reductionnasatSubsonic wind tunnelsnasatFlowmetersnasatJet exhaustnasatWall pressurenasatLoads (forces)nasatData reduction.Subsonic wind tunnels.Flowmeters.Jet exhaust.Wall pressure.Loads (forces)Boney Andy D.1405267Nishikawa HiroakiLangley Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910702734603321Data reduction functions for the Langley 14- by 22-foot subsonic tunnel3481437UNINA