{"id":4568,"date":"2021-06-19T20:26:44","date_gmt":"2021-06-20T01:26:44","guid":{"rendered":"http:\/\/www.orlandobuzzards.org\/?page_id=4568"},"modified":"2022-12-30T21:08:38","modified_gmt":"2022-12-31T02:08:38","slug":"the-physics-of-an-f3j-launch","status":"publish","type":"page","link":"http:\/\/www.orlandobuzzards.org\/?page_id=4568","title":{"rendered":"The Physics of an F3J Launch"},"content":{"rendered":"\n<p><strong>The Physics of an F3J Launch<\/strong>&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; by\nDennis L Harvey<\/p>\n\n\n\n<p><em>This\narticle first appeared in the January 2021 issue of <strong>Model Aviation<\/strong>, the official publication of the Academy of Model\nAeronautics and is reprinted here with permission.&nbsp; This is the longer version of the article\nwhich appeared online with a section that included extra detail and graphs.<\/em><\/p>\n\n\n\n<p>I had been an avid RC sailplane flier during\nthe 1970s but because of my engineering career, I took a very long break.&nbsp; I returned to the sport in 2017 when I moved from\nthe Midwest to central Florida.&nbsp; I was\nwowed by the innovations over those 35 years; from the competitiveness of full\nhouse controls, to miniaturization of electronics, to the extensive use of\ncarbon fiber.&nbsp; <\/p>\n\n\n\n<p>But when I saw my first F3J event, I was\nparticularly fascinated with the launches.&nbsp;\nThey seemed truly brutal.&nbsp; For\none, the F3J winch line is much more elastic than the standard twine thermal\nduration winch lines I used in the past.&nbsp;\nThe dynamics were clearly different.&nbsp;\nIf you haven\u2019t seen an F3J launch, look it up on YouTube.&nbsp; <\/p>\n\n\n\n<p>In an F3J launch, the goal is to get as\nmuch altitude as you need (often up to 250 meters) while staying on the winch line\nas short a time as possible (usually less than 5 seconds).&nbsp; Every second you are on the winch line is a\npoint you can\u2019t make up during the flight or with landing points.&nbsp; As an engineer, I wanted to understand what\nwas happening physically during launch.&nbsp;\nAs I befriended some of the best pilots in my area and did some digging,\nI was surprised to find there is little accessible research on the topic.&nbsp; It didn\u2019t take much arm twisting to put\ntogether a top notch team to take a more scientific look at the subject.<\/p>\n\n\n\n<p><strong>The\nTeam<\/strong><\/p>\n\n\n\n<p>For this experiment, we had some of the\nbest fliers participate by piloting instrumented sailplanes.&nbsp; Three team members have been part of Team\nSoaring USA, representing the United States on the international F3J circuit.&nbsp; Jody Miller took second place at the last\ninternational competition in 2018.&nbsp; Jeff\nDuval is currently the number one USA pilot for the next competition (which was\npostponed this year because of the pandemic).&nbsp;\nGordon Buckland has been on the team numerous times and is a\nquintessential organizer for the sport. Ed Dumas, who drove down from Tennessee\nfor our January 2020 flight weekend, provided invaluable expertise on flying\nand instrumentation.&nbsp; Though I didn\u2019t\nhave the flying credentials of the others, I was quite at home with\nexperimental design as it was often part of my career.<\/p>\n\n\n\n<p><strong>The\nApproach<\/strong><\/p>\n\n\n\n<p>At the core of the experimental design\nwas to measure the sailplane\u2019s energy state as it progressed through the\nlaunch.&nbsp; The total energy of the\nsailplane is the sum of its potential energy (proportional to altitude) and its\nkinetic energy (proportional to speed squared).&nbsp;\nAdditionally, we wanted to video record the launch from onboard in order\nto determine the wing load (based on wing flex) and the angle of the winch line\nand the horizon.&nbsp; Where ever possible, we\ntried to confirm our findings through a secondary measurement or calculation.&nbsp; <strong><br \/>\n<\/strong><\/p>\n\n\n\n<p><strong>A Representative Launch Example<\/strong><\/p>\n\n\n\n<p>To keep this article simple, I will show\nonly one of 26 launches.&nbsp; The launch is\nrepresentative of a high performance F3J launch.&nbsp; Jody Miller was the pilot flying a carbon\nfiber 3.8 meter wing span Xplorer3 F3J model.&nbsp;\nThis is a very common sailplane at F3J events.&nbsp; The temperature was around 80\u00b0 F, our ground\nlevel was approximately 60 feet ASL, and the winds were less than 4 mph.&nbsp; Jody\u2019s launch attained an altitude of 251\nmeters with his total time on the winch line of 4.8 seconds.&nbsp; Flaps were initially set at 15 mm down (12\ndegrees) until the \u201cBucket\u201d phase when they were set 3 mm up for speed.&nbsp; The winch was a standard competition winch with1.32\nmm diameter winch line.<\/p>\n\n\n\n<p><strong>The\nInstrumentation<\/strong>&nbsp; <\/p>\n\n\n\n<p>The key to getting a potential energy\ndetermination was to have an accurate altimeter.&nbsp; Onboard the sailplane, Ed offered up a\nHexpert altimeter which could easily record every tenth of a second.&nbsp; For kinetic energy, we used a FrSky airspeed\nsensor.&nbsp; Unfortunately, its data sampling\nrate was no better than 0.2 seconds. As a result, when graphed every tenth of a\nsecond, the data has a \u201csaw tooth\u201d look to it compared to the Hexpert data. &nbsp;Still, the data was accurate enough to give us\ninsight and could be corroborated by other collected information.<\/p>\n\n\n\n<p>These instruments were mounted\nexternally to the plane as pods shown in Figure 1.&nbsp; The instruments were controlled by a separate\nreceiver so that someone other than the pilot could operate a second\ntransmitter for telemetry, data acquisition.&nbsp;\nAll the pilot had to do was fly the launch.<\/p>\n\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" decoding=\"async\" width=\"800\" height=\"450\" src=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture1-800x450.jpg\" alt=\"\" class=\"wp-image-4561\" srcset=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture1-800x450.jpg 800w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture1-300x169.jpg 300w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture1-150x84.jpg 150w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture1-768x432.jpg 768w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture1-250x141.jpg 250w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture1.jpg 824w\" sizes=\"auto, (max-width: 800px) 100vw, 800px\" \/><\/figure>\n\n\n\n<p>Figure 1.&nbsp; Detachable instrumentation pods. <br \/><\/p>\n\n\n\n<p>Another critical instrument was the onboard video.\u00a0 We chose a camera that is typically used in small drones.\u00a0 Figure 2 shows a Caddx Tarsier installation that is mounted on a carbon fiber blade and sandwiched between the wing panels.\u00a0 The camera looks towards the fuselage to monitor angle of the horizon, angle of the winch line, and wing flex under load.\u00a0 Data was recorded on an SD card which was removed and downloaded every several flights. The video was analyzed one frame at a time and measurements were made on a large screen monitor. Here is a short video of a launch:<\/p>\n\n\n\n<figure class=\"wp-block-embed is-type-video is-provider-youtube wp-block-embed-youtube wp-embed-aspect-16-9 wp-has-aspect-ratio\"><div class=\"wp-block-embed__wrapper\">\n<iframe loading=\"lazy\" title=\"Jody flight F 2020 01 18 wing video\" width=\"870\" height=\"489\" src=\"https:\/\/www.youtube.com\/embed\/-zifKHh7JpM?feature=oembed\" frameborder=\"0\" allow=\"accelerometer; autoplay; clipboard-write; encrypted-media; gyroscope; picture-in-picture\" allowfullscreen><\/iframe>\n<\/div><\/figure>\n\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" decoding=\"async\" width=\"800\" height=\"443\" src=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture2-800x443.jpg\" alt=\"\" class=\"wp-image-4562\" srcset=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture2-800x443.jpg 800w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture2-300x166.jpg 300w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture2-150x83.jpg 150w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture2-768x426.jpg 768w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture2-250x139.jpg 250w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture2.jpg 823w\" sizes=\"auto, (max-width: 800px) 100vw, 800px\" \/><\/figure>\n\n\n\n<p>Figure 2. Under side of the right wing\nshowing the video camera and electronics attached to a carbon fiber blade\nsandwiched between the wing panels.<br \/><\/p>\n\n\n\n<p><strong>Flight\nPath of a F3J Launch<\/strong><\/p>\n\n\n\n<p>Figure 3 shows the distinctly different\nphases of the launch.&nbsp; Let\u2019s go through\neach point on the path.&nbsp; We\u2019ll stick with\nJody\u2019s launch as the example.<\/p>\n\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" decoding=\"async\" width=\"800\" height=\"676\" src=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture3-800x676.jpg\" alt=\"\" class=\"wp-image-4563\" srcset=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture3-800x676.jpg 800w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture3-300x254.jpg 300w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture3-150x127.jpg 150w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture3-768x649.jpg 768w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture3-177x150.jpg 177w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture3.jpg 809w\" sizes=\"auto, (max-width: 800px) 100vw, 800px\" \/><\/figure>\n\n\n\n<p>Figure 3.&nbsp; The flight path during an F3J launch<\/p>\n\n\n\n<p><strong>Point A.&nbsp; <\/strong>Figure\n4 shows Gordon Buckland at the ready to throw the sailplane.&nbsp; He consistently threw the plane at 35 degrees\nto the horizon (as viewed by a ground based video camera aimed at the launch\npoint).&nbsp; It is estimated that Gordon\nrestrained the plane against 600 Newtons of force (135 pounds-force) prior to\nthe throw.&nbsp; This estimate is based on\nforce measurements at the turn around pulley with a digital force meter.<\/p>\n\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" decoding=\"async\" width=\"459\" height=\"585\" src=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture4.jpg\" alt=\"\" class=\"wp-image-4564\" srcset=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture4.jpg 459w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture4-235x300.jpg 235w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture4-118x150.jpg 118w\" sizes=\"auto, (max-width: 459px) 100vw, 459px\" \/><\/figure>\n\n\n\n<p>Figure 4. Gordon Buckland prepared to\nthrow the sailplane at time equals zero.<\/p>\n\n\n\n<p><strong>Point\nB.<\/strong>&nbsp; After the throw, the sailplane establishes\nitself in an equilibrium state to begin the Ascent phase of the launch.&nbsp; Point B happened at time equals 0.3 seconds\nwith a speed of 40 meters per second (89 mph).&nbsp;\nThat represents a g-force acceleration of about 13.5.&nbsp; The speed quickly backed down to around 29\nmeters per second (65 mph) and remained constant till Point C.&nbsp; The plane began the Ascent angled upwards at\n71 degrees to the horizon.&nbsp; Since the sailplane\nmaintained a constant speed, you would expect to see the winch line nearly\nperpendicular to the sailplane and this can be seen in Figure 5.<\/p>\n\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" decoding=\"async\" width=\"461\" height=\"611\" src=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture5.jpg\" alt=\"\" class=\"wp-image-4565\" srcset=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture5.jpg 461w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture5-226x300.jpg 226w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture5-113x150.jpg 113w\" sizes=\"auto, (max-width: 461px) 100vw, 461px\" \/><\/figure>\n\n\n\n<p>Figure 5. This frame grab from the video\nsoon after Point B during the Ascent phase. The winch line is nearly perpendicular\nto the axis of the sailplane. <\/p>\n\n\n\n<p><strong>Point\nC.<\/strong>&nbsp; This is the point of the flight path where\nthe pilot begins to extract remaining energy from the winch line to catapult the\nsailplane forward and achieving the highest speed during the launch.&nbsp; This begins the phase known as the \u201cBucket\u201d.&nbsp; To begin this phase, the pilot retracts the\nflaps and sets them to the speed mode (usually 3 mm up) and pushes the nose\nforward.&nbsp; In Jody\u2019s flight, Point C\nhappened at time equals 4.1 seconds.&nbsp; At\nthis point, he was at an altitude of 125 meters, a speed of 29 meters per\nsecond (65 mph), and the winch line was approximately 45 degrees to the\nhorizon.<\/p>\n\n\n\n<p><strong>Point\nD.<\/strong>&nbsp; At this point, the pilot decides to end the\nenergy extraction of the Bucket phase.&nbsp; In\nJody\u2019s flight, he was in the Bucket for only 0.7 seconds.&nbsp; However, during that time, the sailplane\ndoubled its speed, disengaging from the winch line at a speed of 56 meters per\nsecond (125 mph).&nbsp; Point D happened at\ntime 4.8 seconds.&nbsp; During a contest, this\nis when the timer would begin the stopwatch for the flight.<\/p>\n\n\n\n<p><strong>Point\nE.<\/strong>&nbsp; From Point D to Point E, the pilot is\ncoasting up to a peak altitude since the sailplane is now disengaged from its\nenergy source, the winch line. &nbsp;The\noptimal trajectory is to coast up nearly vertical.&nbsp; When the plane has slowed to near cruise\nspeed, the nose is pushed forward and the plane is leveled off.&nbsp; In Jody\u2019s flight, this happened at time\nequals 9.1 seconds.<\/p>\n\n\n\n<p><strong>The\nEnergy State Graph<\/strong><\/p>\n\n\n\n<p>The prize of the experimentation was the\ncreation of the energy state graph shown in Figure 6.<\/p>\n\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" decoding=\"async\" width=\"800\" height=\"688\" src=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture6-800x688.jpg\" alt=\"\" class=\"wp-image-4566\" srcset=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture6-800x688.jpg 800w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture6-300x258.jpg 300w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture6-150x129.jpg 150w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture6-768x660.jpg 768w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture6-174x150.jpg 174w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture6.jpg 878w\" sizes=\"auto, (max-width: 800px) 100vw, 800px\" \/><\/figure>\n\n\n\n<p>Figure 6.&nbsp; Energy State of the Sailplane.<\/p>\n\n\n\n<p>There are several interesting points to\nnote on the graph.&nbsp; These points were\nconsistent for numerous flights.&nbsp; <\/p>\n\n\n\n<p>First, the initial transfer of energy is\nintense as the sailplane moves towards the quasi-equilibrium state of the Ascent\nwhere the speed remains relatively constant.&nbsp;\nRight after the initial transfer, the sailplane actually gives back\nenergy to the winch system (between time equals 1.0 and 2.0).&nbsp; You will see in the next graph of Wing Load\nFactor, that there is also evidence that the sailplane is helping recharge the\nwinch system to get ready for the Bucket phase and this happens up to about\ntime equals 2.1.<\/p>\n\n\n\n<p>A second interesting point is that after\nthe sailplane is free from the winch line at point D, you would expect the\ntotal energy to remain constant as kinetic energy (speed) is converted to\npotential energy (altitude).&nbsp; However,\nthe total energy decays slightly right after release.&nbsp; It is likely that this is a loss of energy\nfrom drag induced by the high speed (125 mph). Drag is related to the square of\nthe speed so the shape of the decay makes sense.&nbsp; Some of this drag was probably caused by the\nexternal instrumentation.<\/p>\n\n\n\n<p><strong>Wing\nLoad Factor Graph<\/strong><\/p>\n\n\n\n<p>It was possible to measure wing\ndeflection accurately from the wing video.&nbsp;\nIt was a frame by frame process which was laborious.&nbsp; Wing deflection is proportional to the wing\nload or the lift force exerted by the wing.&nbsp;\nTrying to calibrate the information was not practical.&nbsp; Instead, we chose to plot the relative wing\ndeflection as a wing load factor where the maximum load was set at 100%.&nbsp; This yields some valuable insights.&nbsp; Figure 7 shows the Wing Load Factor.<\/p>\n\n\n\n<figure class=\"wp-block-image size-large\"><img loading=\"lazy\" decoding=\"async\" width=\"741\" height=\"681\" src=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture7.jpg\" alt=\"\" class=\"wp-image-4567\" srcset=\"http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture7.jpg 741w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture7-300x276.jpg 300w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture7-150x138.jpg 150w, http:\/\/www.orlandobuzzards.org\/wp-content\/uploads\/2021\/06\/Picture7-163x150.jpg 163w\" sizes=\"auto, (max-width: 741px) 100vw, 741px\" \/><\/figure>\n\n\n\n<p>Figure 7.&nbsp; Wing Load Factor.<\/p>\n\n\n\n<p>Again, you can see that the initial\ntransfer of energy from the winch line to the sailplane generated a spike in\nthe wing load after the throw as the sailplane established its new, quasi-equilibrium\nstate during the Ascent.&nbsp; What this graph\nsuggests is that the force generated by the winch line regained its maximum value\nat time equals 2.1.&nbsp; We hypothesized that\nat that point, if the Bucket was entered, the sailplane could have attained an\naltitude of 215 meters but only have been on the winch line for a total of 2.8\nseconds.&nbsp; That would be worth potentially\n2 extra points for the round which might be golden.<\/p>\n\n\n\n<p>Another insight from a physics\nstandpoint is that the energy extraction from the winch line has similarities\nto a hi-start launch.&nbsp; That being the\ncase, the F3J launch behaves like back to back hi-start launches where the\nhi-start is recharged in between.<\/p>\n\n\n\n<p><strong>In\nConclusion<\/strong><\/p>\n\n\n\n<p>As with any experimentation, you answer\na lot of questions but you raise so many more new ones.&nbsp; The team members mulled over the details of\nthe data and generated a lot of hypotheses to test. &nbsp;We are committed to do another series of tests\nafter the first of the year.&nbsp; We are in\nthe process of amending our instruments and methodology to do so.<\/p>\n\n\n\n<p>A special thanks to my team mates Jody\nMiller, Ed Dumas, Gordon Buckland, and Jeff Duval for this insightful\nexperiment.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>The Physics of an F3J Launch&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; by Dennis L Harvey This article first appeared in the January 2021 issue of Model Aviation, the official publication of the Academy of Model Aeronautics and is reprinted here with permission.&nbsp; This is the longer version of the article which appeared online with a \u2026 <a class=\"continue-reading-link\" href=\"http:\/\/www.orlandobuzzards.org\/?page_id=4568\"> Continue reading <span class=\"meta-nav\">&rarr; <\/span><\/a><\/p>\n","protected":false},"author":4,"featured_media":0,"parent":469,"menu_order":1,"comment_status":"closed","ping_status":"closed","template":"","meta":{"ngg_post_thumbnail":0,"footnotes":""},"class_list":["post-4568","page","type-page","status-publish","hentry"],"_links":{"self":[{"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=\/wp\/v2\/pages\/4568","targetHints":{"allow":["GET"]}}],"collection":[{"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=\/wp\/v2\/pages"}],"about":[{"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=\/wp\/v2\/users\/4"}],"replies":[{"embeddable":true,"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=4568"}],"version-history":[{"count":5,"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=\/wp\/v2\/pages\/4568\/revisions"}],"predecessor-version":[{"id":4836,"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=\/wp\/v2\/pages\/4568\/revisions\/4836"}],"up":[{"embeddable":true,"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=\/wp\/v2\/pages\/469"}],"wp:attachment":[{"href":"http:\/\/www.orlandobuzzards.org\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=4568"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}