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Optical phase distortion due to compressible flow over laser turretsAnalytical models for optical phase distortion due to compressible flow over a laser turret are developed. Phase distortion is calculated for both blunt and small perturbation turrets. For the blunt turret, the Janzen-Rayleigh technique is used to determine the flow field. Phase distortions of 2.2 wavelengths at 3.8 microns are calculated for the blunt turret. For small perturbation turrets, a versatile analytical model is developed for a turret on a fuselage with circular cross section. With a two dimensional Fourier series representation of the turret, any shape can be considered. Both subsonic and supersonic flows can be calculated. Phase distortions of 1.2 wavelengths at 3.8 microns are calculated for one turret at high subsonic Mach number. In addition to being of value for laser turrets, the methods are applicable to reconnaissance aircraft using photographic equipment and cruise missiles using celestial navigation.
Document ID
19800017101
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fuhs, A. E.
(Naval Postgraduate School Monterey, CA, United States)
Fuhs, S. E.
(Calif. Inst. of Tech. Pasadena, United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1980
Publication Information
Publication: NASA. Ames Res. Center Proc. of the Aero-Optics Symp. on Electromagnetic Wave Propagation from Aircraft
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
80N25598
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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