Research output per year
Research output per year
- 28 results
Search results
-
2022
Higher Education Provision in Scotland’s Colleges: A future shaped by new levels of cross-institutional collaboration?
ODonnell, P., 2022, 50 p.Research output: Book/Report › Commissioned report
Open AccessFile100 Downloads (Pure) -
2008
Observations of potential FOD mechanisms for Eurofighter Typhoon
Rae, A., Jan 2008, QinetiQ.Research output: Book/Report › Commissioned report
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2006
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2005
AVERT - Aerodynamic Validation of Emission Reducing Technologies
Rae, A., 2005, European Commission.Research output: Book/Report › Commissioned report
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2004
HELIX Concept 2.1 – Spanwise Fences for Vortex Lift
Rae, A., Nov 2004, QinetiQ.Research output: Book/Report › Commissioned report
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HELIX wind tunnel test report and Reynolds number analysis
Rae, A., Dec 2004, QinetiQ.Research output: Book/Report › Commissioned report
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2003
A Weight Assessment of the Spanwise Fence and Segmented Extension Slotted Flap Concepts
Rae, A., May 2003, QinetiQ.Research output: Book/Report › Commissioned report
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Thrust Reverse Trials on Tornado GR.4
Rae, A., Dec 2003, QinetiQ.Research output: Book/Report › Commissioned report
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2002
An Experimental Study of the Effect of Flow Control Devices on the Efficiency of a Slotted Flap
Rae, A., Feb 2002, QinetiQ.Research output: Book/Report › Commissioned report
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Investigation of the Aerodynamic Interaction between a Moving Freight Train and Station Platform
Rae, A., Jul 2002, QinetiQ.Research output: Book/Report › Commissioned report
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QinetiQ 1 Flight Platform Aerodynamic Analysis
Rae, A., Feb 2002, QinetiQ.Research output: Book/Report › Commissioned report
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Test on the Application of Flow Control to the Swept/Tapered Half-Model, M477, in the QinetiQ 5 Metre Wind Tunnel During July 2001
Rae, A., Feb 2002, QinetiQ.Research output: Book/Report › Commissioned report
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2001
Analysis of the Sensitivity to Reynolds Number of Three Different Flap Designs on the 2-D Endplate Model N15-2
Rae, A., Feb 2001, Defence Evaluation and Research Agency.Research output: Book/Report › Commissioned report
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An Assessment of the Aerodynamic Impact of Airport Buildings on Aircraft Using a Proposed New Runway (28R) at Dublin Airport
Rae, A., Feb 2001, Defence Evaluation and Research Agency.Research output: Book/Report › Commissioned report
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Design, Manufacture and Aerodynamic Assessment of a Wind-Powered Particle Collector
Rae, A., Dec 2001, QinetiQ.Research output: Book/Report › Commissioned report
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Technical Note on the Production of Grids and Aerodynamic Results for a BAC 1-11 Aircraft with Sensor Fairings
Rae, A., Dec 2001, QinetiQ.Research output: Book/Report › Commissioned report
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Technical Note on the Results from the Test at Glasgow University of a 2-D UAV-Type Wing with and without an Ice Shape Affixed to the Leading Edge
Rae, A., Jan 2001, Defence Evaluation and Research Agency.Research output: Book/Report › Commissioned report
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Test on the Application of Flow Control to the Airbus A380 Half-Model, X08, In the QinetiQ 5 Metre Wind Tunnel During October 2001
Rae, A., Oct 2001, QinetiQ.Research output: Book/Report › Commissioned report
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2000
An Assessment of the Aerodynamic Impact of a Proposed Building Development on Aircraft Using Dublin Airport Runway 10/28
Rae, A., Apr 2000, Defence Evaluation and Research Agency.Research output: Book/Report › Commissioned report
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Synopses of the National High-Lift Programme Test and Analytical Reports
Rae, A., Mar 2000, Royal Aircraft Establishment.Research output: Book/Report › Commissioned report
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1999
Aerodynamic Implications of the Addition of a Fairing to the Wing Tip Pod on Nimrod
Rae, A., Aug 1999, Defence Evaluation and Research Agency.Research output: Book/Report › Commissioned report
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Investigation into the Scale Effects Observed on a High-Lift Half-Model (M2296) in the DERA 5m Wind Tunnel
Rae, A., Dec 1999, Defence Evaluation and Research Agency.Research output: Book/Report › Commissioned report
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Particle Image Velocimetry Measurements in the DERA 5m Pressurised Low Speed Wind Tunnel of the Flow Field Behind a Half-Model of the Airbus A310 in a High-Lift Configuration
Rae, A., Jun 1999, Defence Evaluation and Research Agency.Research output: Book/Report › Commissioned report
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1998
Measurements of Flow Angularity in, and Calibration of, the DERA 5 Metre Pressurised Low Speed Wind Tunnel between 1986 and 1992
Rae, A., Jan 1998, Defence Research Agency.Research output: Book/Report › Commissioned report
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1995
Calculation of Wind Tunnel Constraint Using a Hybrid Image and Panel Method
Rae, A., Feb 1995, Defence Research Agency.Research output: Book/Report › Commissioned report
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Correction of Altitude and Airspeed Indication Errors on a Modified Andover (XS790)
Rae, A., Jun 1995, Defence Research Agency.Research output: Book/Report › Commissioned report
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1989
Hawk 0.315 Scale Model – T-45A Database and Development: 5m Wind Tunnel External Data Report No. 42
Rae, A., Sept 1989, Royal Aircraft Establishment.Research output: Book/Report › Commissioned report
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Hawk 0.315 Scale Model – T-45A Database and Development: 5m Wind Tunnel External Data Report No. 43
Rae, A., Nov 1989, Royal Aircraft Establishment.Research output: Book/Report › Commissioned report