Flight simulation and data analysis during a high angle of attack vortex flow control flight test program

Krumenacker, Joseph; Pellicano, Paul

doi:10.2514/6.1992-4108

6th AIAA Biennial Flight Test Conference 1992

DOI: 10.2514/6.1992-4108

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Flight simulation and data analysis during a high angle of attack vortex flow control flight test program

Joseph Krumenacker

Paul Pellicano

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An Investigation of the Fundamental Cause of Asymmetric Separated Flow

Marconi¹

1992

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Public reporting Ou'0*n *or thi» collection of information '» e«i«»«ed, to «.»' »g* \ hour per re»pon»e. including the time for reviewing imtruttion». »eerching emtting d»u »ource». gathering and maintaining the data needed, and completing and reviewing the collection ol information Send comment» regarding thi» Burden estimate or any other »»peel of thu collection of information, including tugcjettion» for reducing thu burden .o wathm^ton Headquarter» Service». Directorate for information Operation» and Report». MM jetfer»on Oavn Highway Suite 1204. Arlington, VA M02-*302, »nö to the Office of Management and Budget. Paperwork «eduction Project (0704-0'86) Wa»nington. DC 2050)

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An Investigation of the Fundamental Cause of Asymmetric Separated Flow

Marconi¹

1992

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Flight Testing of Pneumatic Forebody Vortex Control on the X-29 Technology Demonstrator

Luria¹,

Guyton²

1992

SAE Technical Paper Series

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X-29 High AOA Flight Test Results: An Overview

Smith¹

1993

SAE Technical Paper Series

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Flight simulation and data analysis during a high angle of attack vortex flow control flight test program

Cited by 3 publications

References 0 publications

An Investigation of the Fundamental Cause of Asymmetric Separated Flow

An Investigation of the Fundamental Cause of Asymmetric Separated Flow

Flight Testing of Pneumatic Forebody Vortex Control on the X-29 Technology Demonstrator

X-29 High AOA Flight Test Results: An Overview

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