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A Limited Evaluation of Full Scale Control Surface Deflection Drag (Have FUN)

The Have FUN (FUll Scale Numbers) Test Management Project was conducted at the request of the USAF TPS as an investigation into the drag caused by control surface deflection during dynamic soaring techniques. Forty-three test sorties were performed from 6-23 March 2007 under Job Order Number (JON) M...

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Main Authors:	Reinhardt, R B, Celi, Sean A, Geraghty, Jeffrey T, Stahl, James W, Glover, Victor J, Bowman, Geoffrey G
Format:	Report
Language:	English
Subjects:	Aerodynamics AILERONS ANGLE OF ATTACK ATMOSPHERIC ENERGY EXTRACTION CONTROL SURFACE DEFLECTIONS CONTROL SURFACE DRAG CONTROL SURFACES DEFLECTION DEFLECTION DRAG DRAG DRAG COEFFICIENTS DYNAMIC SOARING ENERGY HEIGHT DATA ENERGY LOSS FLIGHT TESTING Fluid Mechanics GLIDERS Gliders and Parachutes GLIDING HAVE FUN L-23 SUPER BLANIK AIRCRAFT ROLL RATE RUDDERS SAILPLANE ACCELERATIONS SAILPLANE FLIGHT DATA SAILPLANES SOARING MANEUVERS WUTPSM07C0200 YAW YAW RATE
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creator	Reinhardt, R B Celi, Sean A Geraghty, Jeffrey T Stahl, James W Glover, Victor J Bowman, Geoffrey G
description	The Have FUN (FUll Scale Numbers) Test Management Project was conducted at the request of the USAF TPS as an investigation into the drag caused by control surface deflection during dynamic soaring techniques. Forty-three test sorties were performed from 6-23 March 2007 under Job Order Number (JON) M07C0200. The six member Have FUN test team from TPS Class 06B performed the testing at the North Base facilities of Edwards AFB. Flight testing gathered sailplane decelerations during control surface deflections and energy height data during the performance of Dynamic Soaring maneuvers and straight glides. Coefficients of drag for each control surface were determined from minimum sink to maneuvering airspeed of the L-23 Super Blanik. The original document contains color images.
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Forty-three test sorties were performed from 6-23 March 2007 under Job Order Number (JON) M07C0200. The six member Have FUN test team from TPS Class 06B performed the testing at the North Base facilities of Edwards AFB. Flight testing gathered sailplane decelerations during control surface deflections and energy height data during the performance of Dynamic Soaring maneuvers and straight glides. Coefficients of drag for each control surface were determined from minimum sink to maneuvering airspeed of the L-23 Super Blanik. The original document contains color images.</description><language>eng</language><subject>Aerodynamics ; AILERONS ; ANGLE OF ATTACK ; ATMOSPHERIC ENERGY EXTRACTION ; CONTROL SURFACE DEFLECTIONS ; CONTROL SURFACE DRAG ; CONTROL SURFACES ; DEFLECTION ; DEFLECTION DRAG ; DRAG ; DRAG COEFFICIENTS ; DYNAMIC SOARING ; ENERGY HEIGHT DATA ; ENERGY LOSS ; FLIGHT TESTING ; Fluid Mechanics ; GLIDERS ; Gliders and Parachutes ; GLIDING ; HAVE FUN ; L-23 SUPER BLANIK AIRCRAFT ; ROLL RATE ; RUDDERS ; SAILPLANE ACCELERATIONS ; SAILPLANE FLIGHT DATA ; SAILPLANES ; SOARING MANEUVERS ; WUTPSM07C0200 ; YAW ; YAW RATE</subject><creationdate>2007</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA471838$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Reinhardt, R B</creatorcontrib><creatorcontrib>Celi, Sean A</creatorcontrib><creatorcontrib>Geraghty, Jeffrey T</creatorcontrib><creatorcontrib>Stahl, James W</creatorcontrib><creatorcontrib>Glover, Victor J</creatorcontrib><creatorcontrib>Bowman, Geoffrey G</creatorcontrib><creatorcontrib>AIR FORCE FLIGHT TEST CENTER EDWARDS AFB CA</creatorcontrib><title>A Limited Evaluation of Full Scale Control Surface Deflection Drag (Have FUN)</title><description>The Have FUN (FUll Scale Numbers) Test Management Project was conducted at the request of the USAF TPS as an investigation into the drag caused by control surface deflection during dynamic soaring techniques. 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subjects	Aerodynamics AILERONS ANGLE OF ATTACK ATMOSPHERIC ENERGY EXTRACTION CONTROL SURFACE DEFLECTIONS CONTROL SURFACE DRAG CONTROL SURFACES DEFLECTION DEFLECTION DRAG DRAG DRAG COEFFICIENTS DYNAMIC SOARING ENERGY HEIGHT DATA ENERGY LOSS FLIGHT TESTING Fluid Mechanics GLIDERS Gliders and Parachutes GLIDING HAVE FUN L-23 SUPER BLANIK AIRCRAFT ROLL RATE RUDDERS SAILPLANE ACCELERATIONS SAILPLANE FLIGHT DATA SAILPLANES SOARING MANEUVERS WUTPSM07C0200 YAW YAW RATE
title	A Limited Evaluation of Full Scale Control Surface Deflection Drag (Have FUN)
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