Flight test results on the stability and control of the F-15 Quiet Spike aircraft / by Moua, Cheng M.

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In-flight boundary-layer transition on a large flat plate at supersonic speeds / by Banks, D. W.

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Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / by Jones, Daniel S., Bui, Trong T., Ruf, Joseph H.

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Optimal cooperative control synthesis of active displays / by Garg, Sanjay, Schmidt, D. K.

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Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / by Kurtenbach, Frank J., Burcham, Frank W.

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Subsonic flight test evaluation of a propulsion system parameter estimation process for the F-100 engine / by Orme, John S., Gilyard, Glenn B.

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High stability engine control (HISTEC) flight test results / by Southwick, Robert D.

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The high stability engine control (HISTEC) program : flight demonstration phase / by DeLaat, John C.

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