{"id":"v001","input":{"mach":0.78,"pressure_altitude":"35000 ft","temperature":"-54.3 degC"},"expect":{"result.cas.value":264.4201518126049,"result.tas.value":449.6497549943316,"ok":true},"source":"Independent Python implementation of the Gracey (NASA RP-1046) airspeed relations, with supersonic Mach by bisection (tools/vectors/gen_aviation.py)","sourceVersion":"NASA RP-1046 (1980)","tolerance":{"result.cas.value":{"abs":1e-06,"rel":1e-09},"result.tas.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v002","input":{"mach":0.5,"pressure_altitude":"20000 ft","temperature":"-25 degC"},"expect":{"result.cas.value":227.8824882826377,"result.tas.value":306.9259629324943,"ok":true},"source":"Independent Python implementation of the Gracey (NASA RP-1046) airspeed relations, with supersonic Mach by bisection (tools/vectors/gen_aviation.py)","sourceVersion":"NASA RP-1046 (1980)","tolerance":{"result.cas.value":{"abs":1e-06,"rel":1e-09},"result.tas.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v003","input":{"mach":0.25,"pressure_altitude":"3000 ft","temperature":"10 degC"},"expect":{"result.cas.value":156.68032607823287,"result.tas.value":163.92861687617025,"ok":true},"source":"Independent Python implementation of the Gracey (NASA RP-1046) airspeed relations, with supersonic Mach by bisection (tools/vectors/gen_aviation.py)","sourceVersion":"NASA RP-1046 (1980)","tolerance":{"result.cas.value":{"abs":1e-06,"rel":1e-09},"result.tas.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v004","input":{"mach":0.85,"pressure_altitude":"41000 ft","temperature":"-56.5 degC"},"expect":{"result.cas.value":253.3589016265226,"result.tas.value":487.5338283681202,"ok":true},"source":"Independent Python implementation of the Gracey (NASA RP-1046) airspeed relations, with supersonic Mach by bisection (tools/vectors/gen_aviation.py)","sourceVersion":"NASA RP-1046 (1980)","tolerance":{"result.cas.value":{"abs":1e-06,"rel":1e-09},"result.tas.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v005","input":{"mach":1.6,"pressure_altitude":"45000 ft","temperature":"-56.5 degC"},"expect":{"result.cas.value":474.1448587832559,"result.tas.value":917.7107357517558,"ok":true},"source":"Independent Python implementation of the Gracey (NASA RP-1046) airspeed relations, with supersonic Mach by bisection (tools/vectors/gen_aviation.py)","sourceVersion":"NASA RP-1046 (1980)","tolerance":{"result.cas.value":{"abs":1e-06,"rel":1e-09},"result.tas.value":{"abs":1e-06,"rel":1e-09}}}
{"id":"v006","input":{"mach":0.65,"pressure_altitude":"30000 ft","temperature":"-44 degC"},"expect":{"result.cas.value":242.76140116644711,"result.tas.value":383.4244209550141,"ok":true},"source":"Independent Python implementation of the Gracey (NASA RP-1046) airspeed relations, with supersonic Mach by bisection (tools/vectors/gen_aviation.py)","sourceVersion":"NASA RP-1046 (1980)","tolerance":{"result.cas.value":{"abs":1e-06,"rel":1e-09},"result.tas.value":{"abs":1e-06,"rel":1e-09}}}