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Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges by Chu, Julio
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2
High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions by Chu, Julio
Published 1990Call Number: Loading…
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3
Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90° / by Mulcay, William, Chu, Julio
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4
Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges / by Chu, Julio, Luckring, James M.
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5
Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90° by Mulcay, William
Published 1980Other Authors: “…Chu, Julio…”
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6
High Reynolds number test of the Boeing TR77 airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Published 1990Other Authors: “…Chu, Julio…”
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7
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 ̊to 90.̊. by Hultberg, Randy S.
Published 1980Other Authors: “…Chu, Julio…”
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8
Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers / by Tracy, M. B.
Published 1992Other Authors:Call Number: Loading…Search for the full-text version of this title in HathiTrust
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9
Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds by Plentovich, Elizabeth B.
Published 1991Other Authors: “…Chu, Julio…”
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Related Subjects
Reynolds number
Aerodynamics
Spin (Aerodynamics)
Aerodynamic load
Aerodynamics, Transonic
Airplanes
Cavities (Airplanes)
Delta wings
Ground simulators
Leading edges
Mach number
Transonic wind tunnels
Wind tunnel tests
Wind tunnels
Yawing (Aerodynamics)
Aerodynamic measurements
Aerodynamic noise
Bombing, Aerial
Examinations
Low temperature research
Pressure distribution
Private planes
Slender wings
Subsonic speed
Turbulent boundary layer
Vortices
Wind tunnel
Wind tunnel balances
Wings
Wings, Triangular