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| + | {{Template test cases notice}} | ||
| + | ==One of everything== | ||
| + | === (fictional metric)=== | ||
| + | {{testcase table | ||
| + | |ref=<!-- reference -->source name | ||
| + | |prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, | ||
| + | met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
| + | <!-- | ||
| + | General characteristics | ||
| + | --> | ||
| + | |genhide= | ||
| + | |||
| + | |crew=one pilot | ||
| + | |capacity=lots of passengers | ||
| + | |length m=20 | ||
| + | |length ft= | ||
| + | |length in= | ||
| + | |length note=nose probe to tail light | ||
| + | |span m=30 | ||
| + | |span ft= | ||
| + | |span in= | ||
| + | |span note=with extra tips | ||
| + | |upper span m= | ||
| + | |upper span ft= | ||
| + | |upper span in= | ||
| + | |upper span note= | ||
| + | |mid span m= | ||
| + | |mid span ft= | ||
| + | |mid span in= | ||
| + | |mid span note= | ||
| + | |lower span m= | ||
| + | |lower span ft= | ||
| + | |lower span in= | ||
| + | |lower span note= | ||
| + | |swept m=<!-- swing-wings --> | ||
| + | |swept ft=<!-- swing-wings --> | ||
| + | |swept in=<!-- swing-wings --> | ||
| + | |swept note= | ||
| + | |dia m=<!-- airships etc --> | ||
| + | |dia ft=<!-- airships etc --> | ||
| + | |dia in=<!-- airships etc --> | ||
| + | |dia note= | ||
| + | |width m=<!-- if applicable --> | ||
| + | |width ft=<!-- if applicable --> | ||
| + | |width in=<!-- if applicable --> | ||
| + | |width note= | ||
| + | |height m=5 | ||
| + | |height ft= | ||
| + | |height in= | ||
| + | |height note=to top of rudder | ||
| + | |wing area sqm= | ||
| + | |wing area sqft= | ||
| + | |wing area note= | ||
| + | |swept area sqm=<!-- swing-wings --> | ||
| + | |swept area sqft=<!-- swing-wings --> | ||
| + | |swept area note= | ||
| + | |volume m3=<!-- lighter-than-air --> | ||
| + | |volume ft3=<!-- lighter-than-air --> | ||
| + | |volume note= | ||
| + | |aspect ratio=<!-- sailplanes --> | ||
| + | |airfoil=NACA something | ||
| + | |empty weight kg=5000 | ||
| + | |empty weight lb= | ||
| + | |empty weight note=absolutely dry | ||
| + | |gross weight kg=7500 | ||
| + | |gross weight lb= | ||
| + | |gross weight note=all up | ||
| + | |max takeoff weight kg=7800 | ||
| + | |max takeoff weight lb= | ||
| + | |max takeoff weight note=if you must | ||
| + | |fuel capacity=1500 litres | ||
| + | |lift kg=<!-- lighter-than-air --> | ||
| + | |lift lb=<!-- lighter-than-air --> | ||
| + | |lift note= | ||
| + | |more general= | ||
| + | *'''Extra note:''' something else | ||
| + | <!-- | ||
| + | Powerplant | ||
| + | --> | ||
| + | |eng1 number=4 | ||
| + | |eng1 name=Rolls-Whitney AS5 | ||
| + | |eng1 type=turbines | ||
| + | |eng1 kw=<!-- prop engines --> | ||
| + | |eng1 hp=<!-- prop engines --> | ||
| + | |eng1 shp=<!-- prop engines --> | ||
| + | |eng1 kn=5000<!-- jet/rocket engines --> | ||
| + | |eng1 lbf=<!-- jet/rocket engines --> | ||
| + | |eng1 note=at full power | ||
| + | |power original= | ||
| + | |thrust original= | ||
| + | |eng1 kn-ab=1500<!-- afterburners --> | ||
| + | |eng1 lbf-ab=<!-- afterburners --> | ||
| + | |||
| + | |eng2 number= | ||
| + | |eng2 name= | ||
| + | |eng2 type= | ||
| + | |eng2 kw=<!-- prop engines --> | ||
| + | |eng2 hp=<!-- prop engines --> | ||
| + | |eng2 shp=<!-- prop engines --> | ||
| + | |eng2 kn=<!-- jet/rocket engines --> | ||
| + | |eng2 lbf=<!-- jet/rocket engines --> | ||
| + | |eng2 note= | ||
| + | |eng2 kn-ab=<!-- afterburners --> | ||
| + | |eng2 lbf-ab=<!-- afterburners --> | ||
| + | |||
| + | |eng3 number= | ||
| + | |eng3 name= | ||
| + | |eng3 type= | ||
| + | |eng3 kw=<!-- prop engines --> | ||
| + | |eng3 hp=<!-- prop engines --> | ||
| + | |eng3 shp=<!-- prop engines --> | ||
| + | |eng3 kn=<!-- jet/rocket engines --> | ||
| + | |eng3 lbf=<!-- jet/rocket engines --> | ||
| + | |eng3 note= | ||
| + | |eng3 kn-ab=<!-- afterburners --> | ||
| + | |eng3 lbf-ab=<!-- afterburners --> | ||
| + | |more power= | ||
| + | |||
| + | |prop blade number=<!-- propeller aircraft --> | ||
| + | |prop name= | ||
| + | |prop dia m=<!-- propeller aircraft --> | ||
| + | |prop dia ft=<!-- propeller aircraft --> | ||
| + | |prop dia in=<!-- propeller aircraft --> | ||
| + | |prop dia note= | ||
| + | |||
| + | |rot number=<!-- helicopters --> | ||
| + | |rot dia m=<!-- helicopters --> | ||
| + | |rot dia ft=<!-- helicopters --> | ||
| + | |rot dia in=<!-- helicopters --> | ||
| + | |rot area sqm=<!-- helicopters --> | ||
| + | |rot area sqft=<!-- helicopters --> | ||
| + | |rot area note= | ||
| + | <!-- | ||
| + | Performance | ||
| + | --> | ||
| + | |perfhide= | ||
| + | |||
| + | |max speed kmh=500 | ||
| + | |max speed mph= | ||
| + | |max speed kts= | ||
| + | |max speed note=flat out | ||
| + | |max speed mach=<!-- supersonic aircraft --> | ||
| + | |cruise speed kmh=350 | ||
| + | |cruise speed mph= | ||
| + | |cruise speed kts= | ||
| + | |cruise speed note=nice and gentle | ||
| + | |stall speed kmh=160 | ||
| + | |stall speed mph= | ||
| + | |stall speed kts= | ||
| + | |stall speed note=full flaps and praying | ||
| + | |never exceed speed kmh=800 | ||
| + | |never exceed speed mph= | ||
| + | |never exceed speed kts= | ||
| + | |never exceed speed note=on a good day | ||
| + | |minimum control speed kmh=155 | ||
| + | |minimum control speed mph= | ||
| + | |minimum control speed kts= | ||
| + | |minimum control speed note=whatever this means | ||
| + | |range km=1000 | ||
| + | |range miles= | ||
| + | |range nmi= | ||
| + | |range note=full tank | ||
| + | |combat range km=500 | ||
| + | |combat range miles= | ||
| + | |combat range nmi= | ||
| + | |combat range note=travelling light | ||
| + | |ferry range km=2000 | ||
| + | |ferry range miles= | ||
| + | |ferry range nmi= | ||
| + | |ferry range note=with extra tanks | ||
| + | |endurance=<!-- if range unknown --> | ||
| + | |ceiling m=10000 | ||
| + | |ceiling ft= | ||
| + | |ceiling note=half full | ||
| + | |g limits=<!-- aerobatic --> | ||
| + | |roll rate=<!-- aerobatic --> | ||
| + | |glide ratio=<!-- sailplanes --> | ||
| + | |climb rate ms=10 | ||
| + | |climb rate ftmin= | ||
| + | |climb rate note=kind of gentle | ||
| + | |time to altitude= | ||
| + | |sink rate ms=<!-- sailplanes --> | ||
| + | |sink rate ftmin=<!-- sailplanes --> | ||
| + | |sink rate note= | ||
| + | |lift to drag= | ||
| + | |wing loading kg/m2= | ||
| + | |wing loading lb/sqft= | ||
| + | |wing loading note= | ||
| + | |disk loading kg/m2= | ||
| + | |disk loading lb/sqft= | ||
| + | |disk loading note= | ||
| + | |fuel consumption kg/km=22 | ||
| + | |fuel consumption lb/mi= | ||
| + | |power/mass= | ||
| + | |thrust/weight= | ||
| − | == | + | |more performance= |
| − | {{ | + | <!-- |
| + | Armament | ||
| + | --> | ||
| + | |armament=<!-- add bulletted list here or if you want to use the following | ||
| + | specific parameters, remove this parameter--> | ||
| + | |guns= | ||
| + | |bombs= | ||
| + | |rockets= | ||
| + | |missiles= | ||
| + | |hardpoints= | ||
| + | |hardpoint capacity= | ||
| + | |hardpoint rockets= | ||
| + | |hardpoint missiles= | ||
| + | |hardpoint bombs= | ||
| + | |hardpoint other= | ||
| + | |||
| + | |avionics= | ||
| + | }} | ||
| + | === (fictional imp)=== | ||
| + | but with only metric values in the params | ||
| + | {{testcase table | ||
|ref=<!-- reference -->source name | |ref=<!-- reference -->source name | ||
| − | |prime units?= | + | |prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, |
met(ric) first for all others. You MUST choose a format, or no specifications will show --> | met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
<!-- | <!-- | ||
| Line 195: | Line 410: | ||
|more performance= | |more performance= | ||
| + | <!-- | ||
| + | Armament | ||
| + | --> | ||
| + | |armament=<!-- add bulletted list here or if you want to use the following | ||
| + | specific parameters, remove this parameter--> | ||
| + | |guns= | ||
| + | |bombs= | ||
| + | |rockets= | ||
| + | |missiles= | ||
| + | |hardpoints= | ||
| + | |hardpoint capacity= | ||
| + | |hardpoint rockets= | ||
| + | |hardpoint missiles= | ||
| + | |hardpoint bombs= | ||
| + | |hardpoint other= | ||
| + | |||
| + | |avionics= | ||
| + | }} | ||
| + | === (fictional in knots)=== | ||
| + | but only metric in params | ||
| + | |||
| + | {{testcase table | ||
| + | |ref=<!-- reference -->source name | ||
| + | |prime units?=kts<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, | ||
| + | met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
| + | <!-- | ||
| + | General characteristics | ||
| + | --> | ||
| + | |genhide= | ||
| + | |||
| + | |crew=one pilot | ||
| + | |capacity=lots of passengers | ||
| + | |length m=20 | ||
| + | |length ft= | ||
| + | |length in= | ||
| + | |length note=nose probe to tail light | ||
| + | |span m=30 | ||
| + | |span ft= | ||
| + | |span in= | ||
| + | |span note=with extra tips | ||
| + | |upper span m= | ||
| + | |upper span ft= | ||
| + | |upper span in= | ||
| + | |upper span note= | ||
| + | |mid span m= | ||
| + | |mid span ft= | ||
| + | |mid span in= | ||
| + | |mid span note= | ||
| + | |lower span m= | ||
| + | |lower span ft= | ||
| + | |lower span in= | ||
| + | |lower span note= | ||
| + | |swept m=<!-- swing-wings --> | ||
| + | |swept ft=<!-- swing-wings --> | ||
| + | |swept in=<!-- swing-wings --> | ||
| + | |swept note= | ||
| + | |dia m=<!-- airships etc --> | ||
| + | |dia ft=<!-- airships etc --> | ||
| + | |dia in=<!-- airships etc --> | ||
| + | |dia note= | ||
| + | |width m=<!-- if applicable --> | ||
| + | |width ft=<!-- if applicable --> | ||
| + | |width in=<!-- if applicable --> | ||
| + | |width note= | ||
| + | |height m=5 | ||
| + | |height ft= | ||
| + | |height in= | ||
| + | |height note=to top of rudder | ||
| + | |wing area sqm= | ||
| + | |wing area sqft= | ||
| + | |wing area note= | ||
| + | |swept area sqm=<!-- swing-wings --> | ||
| + | |swept area sqft=<!-- swing-wings --> | ||
| + | |swept area note= | ||
| + | |volume m3=<!-- lighter-than-air --> | ||
| + | |volume ft3=<!-- lighter-than-air --> | ||
| + | |volume note= | ||
| + | |aspect ratio=<!-- sailplanes --> | ||
| + | |airfoil=NACA something | ||
| + | |empty weight kg=5000 | ||
| + | |empty weight lb= | ||
| + | |empty weight note=absolutely dry | ||
| + | |gross weight kg=7500 | ||
| + | |gross weight lb= | ||
| + | |gross weight note=all up | ||
| + | |max takeoff weight kg=7800 | ||
| + | |max takeoff weight lb= | ||
| + | |max takeoff weight note=if you must | ||
| + | |fuel capacity=1500 litres | ||
| + | |lift kg=<!-- lighter-than-air --> | ||
| + | |lift lb=<!-- lighter-than-air --> | ||
| + | |lift note= | ||
| + | |more general= | ||
| + | *'''Extra note:''' something else | ||
| + | <!-- | ||
| + | Powerplant | ||
| + | --> | ||
| + | |eng1 number=4 | ||
| + | |eng1 name=Rolls-Whitney AS5 | ||
| + | |eng1 type=turbines | ||
| + | |eng1 kw=<!-- prop engines --> | ||
| + | |eng1 hp=<!-- prop engines --> | ||
| + | |eng1 shp=<!-- prop engines --> | ||
| + | |eng1 kn=5000<!-- jet/rocket engines --> | ||
| + | |eng1 lbf=<!-- jet/rocket engines --> | ||
| + | |eng1 note=at full power | ||
| + | |power original= | ||
| + | |thrust original= | ||
| + | |eng1 kn-ab=<!-- afterburners --> | ||
| + | |eng1 lbf-ab=<!-- afterburners --> | ||
| + | |||
| + | |eng2 number= | ||
| + | |eng2 name= | ||
| + | |eng2 type= | ||
| + | |eng2 kw=<!-- prop engines --> | ||
| + | |eng2 hp=<!-- prop engines --> | ||
| + | |eng2 shp=<!-- prop engines --> | ||
| + | |eng2 kn=<!-- jet/rocket engines --> | ||
| + | |eng2 lbf=<!-- jet/rocket engines --> | ||
| + | |eng2 note= | ||
| + | |eng2 kn-ab=<!-- afterburners --> | ||
| + | |eng2 lbf-ab=<!-- afterburners --> | ||
| + | |||
| + | |eng3 number= | ||
| + | |eng3 name= | ||
| + | |eng3 type= | ||
| + | |eng3 kw=<!-- prop engines --> | ||
| + | |eng3 hp=<!-- prop engines --> | ||
| + | |eng3 shp=<!-- prop engines --> | ||
| + | |eng3 kn=<!-- jet/rocket engines --> | ||
| + | |eng3 lbf=<!-- jet/rocket engines --> | ||
| + | |eng3 note= | ||
| + | |eng3 kn-ab=<!-- afterburners --> | ||
| + | |eng3 lbf-ab=<!-- afterburners --> | ||
| + | |more power= | ||
| + | |||
| + | |prop blade number=<!-- propeller aircraft --> | ||
| + | |prop name= | ||
| + | |prop dia m=<!-- propeller aircraft --> | ||
| + | |prop dia ft=<!-- propeller aircraft --> | ||
| + | |prop dia in=<!-- propeller aircraft --> | ||
| + | |prop dia note= | ||
| + | |||
| + | |rot number=<!-- helicopters --> | ||
| + | |rot dia m=<!-- helicopters --> | ||
| + | |rot dia ft=<!-- helicopters --> | ||
| + | |rot dia in=<!-- helicopters --> | ||
| + | |rot area sqm=<!-- helicopters --> | ||
| + | |rot area sqft=<!-- helicopters --> | ||
| + | |rot area note= | ||
| + | <!-- | ||
| + | Performance | ||
| + | --> | ||
| + | |perfhide= | ||
| + | |||
| + | |max speed kmh=500 | ||
| + | |max speed mph= | ||
| + | |max speed kts= | ||
| + | |max speed note=flat out | ||
| + | |max speed mach=<!-- supersonic aircraft --> | ||
| + | |cruise speed kmh=350 | ||
| + | |cruise speed mph= | ||
| + | |cruise speed kts= | ||
| + | |cruise speed note=nice and gentle | ||
| + | |stall speed kmh=160 | ||
| + | |stall speed mph= | ||
| + | |stall speed kts= | ||
| + | |stall speed note=full flaps and praying | ||
| + | |never exceed speed kmh=800 | ||
| + | |never exceed speed mph= | ||
| + | |never exceed speed kts= | ||
| + | |never exceed speed note=on a good day | ||
| + | |minimum control speed kmh=155 | ||
| + | |minimum control speed mph= | ||
| + | |minimum control speed kts= | ||
| + | |minimum control speed note=whatever this means | ||
| + | |range km=1000 | ||
| + | |range miles= | ||
| + | |range nmi= | ||
| + | |range note=full tank | ||
| + | |combat range km= | ||
| + | |combat range miles= | ||
| + | |combat range nmi= | ||
| + | |combat range note= | ||
| + | |ferry range km= | ||
| + | |ferry range miles= | ||
| + | |ferry range nmi= | ||
| + | |ferry range note= | ||
| + | |endurance=<!-- if range unknown --> | ||
| + | |ceiling m=10000 | ||
| + | |ceiling ft= | ||
| + | |ceiling note= | ||
| + | |g limits=<!-- aerobatic --> | ||
| + | |roll rate=<!-- aerobatic --> | ||
| + | |glide ratio=<!-- sailplanes --> | ||
| + | |climb rate ms=10 | ||
| + | |climb rate ftmin= | ||
| + | |climb rate note=kind of gentle | ||
| + | |time to altitude= | ||
| + | |sink rate ms=<!-- sailplanes --> | ||
| + | |sink rate ftmin=<!-- sailplanes --> | ||
| + | |sink rate note= | ||
| + | |lift to drag= | ||
| + | |wing loading kg/m2= | ||
| + | |wing loading lb/sqft= | ||
| + | |wing loading note= | ||
| + | |disk loading kg/m2= | ||
| + | |disk loading lb/sqft= | ||
| + | |disk loading note= | ||
| + | |fuel consumption kg/km=22 | ||
| + | |fuel consumption lb/mi=23 | ||
| + | |power/mass= | ||
| + | |thrust/weight= | ||
| + | |||
| + | |more performance=*'''Something else:''' but nothing special | ||
<!-- | <!-- | ||
Armament | Armament | ||
| Line 215: | Line 645: | ||
==Testing auto reversing (MET, no inches)== | ==Testing auto reversing (MET, no inches)== | ||
| − | {{ | + | {{testcase table |
|ref=<!-- reference --> | |ref=<!-- reference --> | ||
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> | |prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
| Line 406: | Line 836: | ||
==Specifications== | ==Specifications== | ||
| − | {{ | + | {{testcase table |
|ref=British Civil Aircraft 1919-72<ref>Jackson 1973 p.296 </ref> | |ref=British Civil Aircraft 1919-72<ref>Jackson 1973 p.296 </ref> | ||
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> | |prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
| Line 505: | Line 935: | ||
==prop testing section== | ==prop testing section== | ||
===no number value test=== | ===no number value test=== | ||
| − | {{ | + | {{testcase table |
|ref= | |ref= | ||
|prime units?=met | |prime units?=met | ||
| Line 516: | Line 946: | ||
}} | }} | ||
===diameter test=== | ===diameter test=== | ||
| − | {{ | + | {{testcase table |
|ref= | |ref= | ||
|prime units?=met | |prime units?=met | ||
| Line 528: | Line 958: | ||
===type test=== | ===type test=== | ||
| − | {{ | + | {{testcase table |
|ref= | |ref= | ||
|prime units?=met | |prime units?=met | ||
| Line 536: | Line 966: | ||
|props per engine=2 | |props per engine=2 | ||
|prop note=<ref>something</ref> | |prop note=<ref>something</ref> | ||
| + | |||
| + | }} | ||
| + | ===type test=== | ||
| + | |||
| + | {{testcase table | ||
| + | |ref= | ||
| + | |prime units?=met | ||
| + | |||
| + | |prop name=Rotol reversing propeller | ||
| + | |||
| + | }} | ||
| + | |||
| + | {{testcase table | ||
| + | |ref= | ||
| + | |prime units?=met | ||
| + | |||
| + | |prop blade number=317 | ||
| + | |prop name=Rotol reversing propeller | ||
}} | }} | ||
| Line 542: | Line 990: | ||
===Rotodyne - aircraft specifications template=== | ===Rotodyne - aircraft specifications template=== | ||
[[Image:Fairey Rotodyne three-view silhouette.png|right|300px|Fairey Rotodyne 3-view]] | [[Image:Fairey Rotodyne three-view silhouette.png|right|300px|Fairey Rotodyne 3-view]] | ||
| − | + | {{testcase table|_template=Aircraft specifications|_template2=Aircraft specifications/sandbox | |
| − | {{ | ||
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | <!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] --> | ||
<!-- please answer the following questions --> | <!-- please answer the following questions --> | ||
| Line 592: | Line 1,039: | ||
|power/mass alt=280 W/kg | |power/mass alt=280 W/kg | ||
}} | }} | ||
| + | |||
===Rotodyne - this template=== | ===Rotodyne - this template=== | ||
| − | {{ | + | {{testcase table |
|ref=<!-- reference --> | |ref=<!-- reference --> | ||
|prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> | |prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> | ||
| Line 607: | Line 1,055: | ||
|length in=8 | |length in=8 | ||
|length note= | |length note= | ||
| − | |||
| − | |||
|span m= | |span m= | ||
|span ft=90 | |span ft=90 | ||
| Line 638: | Line 1,084: | ||
|width note= | |width note= | ||
|height m= | |height m= | ||
| − | |height ft= | + | |height ft=22 |
| − | |height in= | + | |height in=2 |
|height note= | |height note= | ||
|wing area sqm= | |wing area sqm= | ||
| Line 769: | Line 1,215: | ||
|lift to drag= | |lift to drag= | ||
|wing loading kg/m2= | |wing loading kg/m2= | ||
| − | |wing loading lb/sqft= | + | |wing loading lb/sqft= |
|wing loading note= | |wing loading note= | ||
|disk loading kg/m2= | |disk loading kg/m2= | ||
| − | |disk loading lb/sqft= | + | |disk loading lb/sqft=5.2 |
|disk loading note= | |disk loading note= | ||
| − | |more performance= | + | |more performance= |
| − | + | * '''Power/mass (prop):''' {{convert|0.17|hp/lb|abbr=on}} | |
|power/mass met= | |power/mass met= | ||
|power/mass note= | |power/mass note= | ||
| Line 782: | Line 1,228: | ||
}} | }} | ||
| + | |||
| + | ==Swept parm== | ||
| + | {{Testcase table |_class=wikitable |_showcode=true |prime units?=met |genhide=Y |span m=20 }} | ||
| + | ---- | ||
| + | {{Testcase table |_class=wikitable |_showcode=true |prime units?=met |genhide=Y |span m=20 |swept m=12 }} | ||
| + | ---- | ||
| + | {{Testcase table |_class=wikitable |_showcode=true |prime units?=met |genhide=Y |upper span m=15 |lower span m=20 }} | ||
| + | ---- | ||
| + | {{Testcase table |_class=wikitable |_showcode=true |prime units?=met |genhide=Y |upper span m=15 |lower span m=20 |swept m=12 }} | ||
==ref dump== | ==ref dump== | ||
{{reflist}} | {{reflist}} | ||
Latest revision as of 13:53, 18 October 2020
- REDIRECT Template:Testcases notice
- From a page move: This is a redirect from a page that has been moved (renamed). This page was kept as a redirect to avoid breaking links, both internal and external, that may have been made to the old page name.
Contents
One of everything
(fictional metric)
(fictional imp)
but with only metric values in the params Template:Testcase table
(fictional in knots)
but only metric in params