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High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test by Cobleigh, Brent R.
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2
Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack by Cobleigh, Brent R.
Published 2001Call Number: Loading…
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3
Water tunnel flow visualization study of a 4.4% scale X-31 forebody by Cobleigh, Brent R.
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4
Development of the X-33 aerodynamic uncertainty model by Cobleigh, Brent R.
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5
Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack / by Cobleigh, Brent R., Croom, Mark A.
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6
Design and calibration of the X-33 flush airdata sensing (FADS) system / by Whitmore, Stephen A., Cobleigh, Brent R., Haering, Edward A.
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7
Flush airdata sensing (FADS) system calibration procedures and results for blunt forebodies
Published 1999Other Authors: “…Cobleigh, Brent R.…”
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8
Controlling forebody asymmetries in flight experience with boundary layer transition strips / by Fisher, David F.
Published 1994Other Authors: “…Cobleigh, Brent R.…”
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9
Aerodynamic parameters of High-Angle-of-Attack Research Vehicle (HARV) estimated from flight data by Klein, Vladislav
Published 1990Other Authors:Call Number: Loading…
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10
Design and calibration of the X-33 flush airdata sensing (FADS) system by Whitmore, Stephen A.
Published 1998Other Authors: “…Cobleigh, Brent R.…”
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Related Subjects
Forebodies
Asymmetry
Water tunnel tests
Yawing moments
Angle of attack
Calibrating
Flight envelopes
Wind tunnel tests
X-31 aircraft
X-33 reusable launch vehicle
Aerodynamic characteristics
Aerodynamics
Aircraft maneuvers
Angle of attack (Aerodynamics)
Data systems
Design
Detection
Dynamic stability
Flight characteristics
Flight control
Flight tests
Flow visualization
Hypersonics
Lifting bodies
Mathematical models
Monte Carlo method
Pressure measurement
Remote sensing
Reusable launch vehicles
Space Shuttle orbiters