Integrated air data sensors

Aeronautical Journal

Volumn 105, Issue 1046, 2001, Pages 223-229

  Menzies, M A ^a  

^a New Business Development   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0345771686     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S000192400002546X     Document Type: Article

References (9)

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2. COULTHARD, W.H. Aircraft Instrument Design, Sir Isaac Pitman and Sons, Bath, 1952, pp 62-72.
3. HOWARD, W. Reduced vertical separation minimum (RVSM). Airliner. Jul-Sep Issue, 1996, pp R-15.
4. GOWEN, F.E. and PERKINS, E.W. Drag of circular cylinders for a wide range of Reynolds numbers and Mach numbers, National Advisory Committee for Aeronautics Technical Note 2960, Moffett Field, California, 1953.
5. MENZIES, M.A. Development and design of the multifunction probe-a summary of F-16 flight test data. Avionics Specialties Research Report. 1998.
6. MENZIES, M.A. Icing tunnel test F-16 to MFP comparison, Avionics Specialties Test Report, conducted at LeCleric Icing Wind Tunnel, New York, 1998.
7. BALTINS, G.U., BOYLE, R.W., MASON, D.G., MOORE, H.M., DEBOW OWEN, A. and SHARP, J.A. Combined aircraft angle of attack and dynamic/static pressure sensor assembly, United Slates Patent, 5,544,526, Avionics Specialties Inc, 13 August 1996.
8. MENZIES, M.A., BALTINS, G.U. and Martin, D.N. Improvements to multifunction aircraft probes, United States Patent, 6,012,331. Avionics Specialties Inc, 2 July 1998.
9. MENZIES, M.A. and BALTINS, G.U. Aircraft probe with integral air temperature sensor, United States Patent, 6,076,963, Avionics Specialties Inc, 29 September 1998.