Theoretical and Experimental Study of Supersonic Steady Flow around Inclined Bodies of Revolution von RAKICH, JOHN V, CLEARY, JOSEPH W

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Effects of angle of attack and bluntness on the hypersonic flow over a 15 ̊semiapex cone in helium / Joseph W. Cleary and Charles E. Duller von Cleary, Joseph W

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Approximation for distribution of flow properties in the angle-of-attack plane of conical flows / Joseph W. Cleary von Cleary, Joseph W

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Flow over an all-body hypersonic aircraft - Experiment and computation von Lockman, William K, Lawrence, Scott L, Cleary, Joseph W

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Wedge and cone theory for m infinity equals infinity von CLEARY, JOSEPH W

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Adapter for a jacking device von JOSEPH W. CLEARY

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ADAPTER FOR A JACKING DEVICE von CLEARY, JOSEPH, W

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Adapter for a jacking device von CLEARY, JOSEPH W

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Experimental and computational flow-field results for an all-body hypersonic aircraft von Cleary, Joseph W.

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Experimental aerothermodynamic research of hypersonic aircraft von Cleary, Joseph W.

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Experimental aerothermodynamic research of hypersonic aircraft von Cleary, Joseph W.

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Effects of angle of attack and bluntness on laminar heating-rate distributions of a 15 ̊cone at a Mach number of 10.6 / by Joseph W. Cleary : v.5450 von Cleary, Joseph W

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An experimental and theoretical investigation of the pressure distribution and flow fields of blunted cones at hypersonic Mach number / by Joseph W. Cleary von Cleary, Joseph W

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The Transonic Aerodynamic Characteristics of Structurally Related Wings of Low Aspect Ratio Having a Spanwise Variation in Thickness Ratio-transonic Bump Technique von Cleary, Joseph W

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Theoretical and experimental study of supersonic steady flow around inclined bodies of revolution von RAKICH, JOHN V., CLEARY, JOSEPH W.

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Wind-tunnel Investigation of a 45 Degree Sweptback Wing Having a Symmetrical Root and a Highly Cambered Tip, Including the Effects of Fences and Lateral Controls von Cleary, Joseph W, Boddy, Lee E

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The Effects at Transonic Speeds of Thickening the Trailing Edge of a Wing with a 4-percent-thick Circular-arc Airfoil von Cleary, Joseph W, Stevens, George L

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An Investigation of the Aerodynamic Characteristics in Pitch of an XB-52 Airplane Model in a High-Speed Wind Tunnel von Cleary, Joseph W., Coe, Charles F.

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High-speed Aerodynamic Characteristics of a Lateral-control Model III : Section Characteristics, Fence Studies, and Tabulated Pressure Coefficients with Modified NACA 0012-64 Secti... von Krumm, Walter J, Cleary, Joseph W

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Wind-tunnel Tests of a 0.16-scale Model of the X-3 Airplane at High Subsonic Speeds : Wing and Fuselage Pressure Distribution von Cleary, Joseph W, Mellenthin, Jack A

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