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Title
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System Description and Performance Data for the USAF/CAL Variable Stability T-33 Airplane
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Date
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1970
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Index Abstract
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Coming Soon
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Photo Quality
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Complete
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Report Number
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AFFDL TR 70-71
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Creator
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Hall, G. Warren
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Huber, Ronald W.
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Corporate Author
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Cornell Aeronautical Lab Inc Buffalo N Y
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Laboratory
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Air Force Flight Dynamics Laboratory
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Extent
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332
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Identifier
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AD0876626
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Distribution Classification
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1
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Contract
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F33615-69-C-1664
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DoD Project
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8219
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DoD Task
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821905
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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AFWAL LTR
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Special Scanning Requirements
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Fold out pages
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Date Modified
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Scanned by request 2/7/2006 submitted by Athena Controls (Other Industry - Domestic)
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Abstract
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The USAF/CAL variable stability T-33 airplane is a jet trainer which has been extensively modified for use as a research vehicle. A response-feedback system allows the normal T-33 derivatives to be augmented so that handling qualities of existing airplanes, future airplanes, or hypothetical configurations may be simulated in flight or in a fixed-base ground simulator. The report attempts to provide an updated functional description of the variable stability T-33. The information is presented for setting up a simulation program and for performing calibration procedures. A brief description of the equipment and airplane systems is also included.
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Report Availability
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Full text available
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Date Issued
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1970-08
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Provenance
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AFRL/VACA
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Lockheed Martin Missiles & Fire Control
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Type
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report
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Format
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1 online resource
AFFDLTR70-071.pdf