Stephen A. Whitmore

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Development of a closed-loop strap down attitude system for an ultrahigh altitude flight experiment

by Stephen A. Whitmore First published in 1997 — 5 editions

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Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness

by Stephen A. Whitmore First published in 2001 — 4 editions

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Air data position-error calibration using state reconstruction techniques

by Stephen A. Whitmore First published in 1984 — 4 editions

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In-flight demonstration of a Real-Time Flush Airdata Sensing (RT-FADS) system

by Stephen A. Whitmore First published in 1995 — 3 editions

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Formulation and implementation of nonstationary adaptive estimation algorithm with applications to air-data reconstruction

by Stephen A. Whitmore First published in 1985 — 2 editions

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Failure detection and fault management techniques for a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system

by Stephen A. Whitmore First published in 1992 — 2 editions

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A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program

by Stephen A. Whitmore First published in 1999 — 1 edition

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Design and calibration of the X-33 flush airdata sensing (FADS) system

by Stephen A. Whitmore First published in 1998 — 1 edition

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The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system

by Stephen A. Whitmore First published in 1991 — 1 edition

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Measurement uncertainty and a feasibility study of a flush airdata system for a hypersonic flight experiment

by Stephen A. Whitmore First published in 1994 — 1 edition

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An optimal deconvolution method for reconstructing pneumatically distorted near-field sonic boom pressure measurements

by Stephen A. Whitmore First published in 1996 — 1 edition

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Real-time method for estimating viscous forebody drag coefficients

by Stephen A. Whitmore First published in 2000 — 1 edition

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Compensating for pneumatic distortion in pressure sensing devices

by Stephen A. Whitmore First published in 1990 — 1 edition

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Preliminary results from a subsonic high angle-of-attack flush airdata sensing (HI-FADS) system: design, calibration, and flight test evaluation

by Stephen A. Whitmore First published in 1990 — 1 edition

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A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients

by Stephen A. Whitmore First published in 1996 — 1 edition

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Development of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system

by Stephen A. Whitmore First published in 1991 — 1 edition

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OLID: OL4837354A

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Created September 19, 2008
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September 19, 2008

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Stephen A. Whitmore

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