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1by Mutchler, Mack SteeleSubjects: “...Wind tunnels -- Testing...”
Published 2016
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2by Engel, Mark A.“...<p>A 3 'x2' subsonic wind tunnel has been constructed and calibrated. The flow in the wind tunnel...”
Published 2014
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3by Anderson, Euell ClaySubjects: “...Supersonic wind tunnels -- Design...”
Published 2016
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4by Sumantran, V.Subjects: “...Wind tunnels -- Flow visualization...”
Published 2014
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5by Perkins, John NobleSubjects: “...Rocket engines -- Fuel systems...”
Published 2014
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7by Hetreed, Christopher F.Subjects: “...Rocket engines -- Fuel systems...”
Published 2014
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8by Kim, Sangho“... experimentally in a water tunnel for two low speed cases. A wing consisting of a 3 : 2 elliptical nose...”
Published 2014
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9by Wei, Chunghwa“... evaluated in a wind tunnel test. The wind tunnel test showed a non-linear and a non-cosine behavior...”
Published 2014
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10by Novean, Michael George Bernard“... of engineering plastics and short beam length provide high frequency response and make the beam stiff so...”
Published 2014
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11by Faery, Henry Frederick“...Wind tunnel experiments have been conducted on six different wingtip configurations to determine...”
Published 2014
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12by Blohm, Raymond William“...' stability wind tunnel. Summaries of the characteristics of the flow over the unheated wing...”
Published 2015
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13by Daffan, Edward Bruce“... subsonic tunnel at free-stream Re<sub>D</sub> ≃ 4.4 x 10⁵. The addition of the appendage substantially...”
Published 2017
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14by Lee, Heehwan“... in a wind tunnel with yaw-head and hot-wire probes at three different Reynolds numbers, the highest...”
Published 2017
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15by Squire, Daniel E.“... firings. The SRM was simulated by water flow through a plexiglas model mounted in a water tunnel. Dye...”
Published 2014
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16by Liu, Ding-Jen“... system was designed and developed to be used in the Virginia Tech Stability wind tunnel. Flowfield...”
Published 2014
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17by Holland, Scott D.“... DTNSRDC 4767A marine propeller was conducted in the VPI Stability tunnel at an advance ratio of 0.95 in a...”
Published 2015
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18by Rife, Michael C.“...Velocity and pressure fluctuations were measured in a wind tunnel in the plane of symmetry in front...”
Published 2014
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19by McGrath, Brian E.“..., conducted in the Virginia Tech low speed boundary layer wind tunnel, covered the effects of zero...”
Published 2020
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20by Paik, Seung Woock“.... Tests were conducted in the Virginia Tech supersonic wind tunnel. The nominal Mach number was 2.4...”
Published 2014
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