In flight the arrow oscillates in pitch, one cycle every fourteen to twenty-two metres, and the waviness shows mostly over the first stretch

8 studies

ForContextAgainst2010201220142016201820202022202420262017, for, n = 12011, for2014, context2016, for2018, for2019, for2020, context2020, for2022, context
Each circle is a study: its position gives the year, its row whether it is for, against or context, its size how many participants it measured. Light circles are studies on other populations or without archers.

The frequency of the arrow's oscillation in flight, study by study

Each row is one arrow or one flight condition, and the dot is the frequency of the oscillation; no study reports an interval, so there are no whiskers. The rows marked "calculation" are simulations by the Tokyo group on A/C/E arrows treated as rigid bodies, with no flexing of the shaft, using coefficients measured by the same group: launched at 60 metres per second for Miyazaki 2017, at 57.3 with a 3 metre per second side, head or tail wind for Ortiz 2018, and at 56 for Ortiz 2020. Ortiz 2020 is context because its measurement in flight concerns drag, not the oscillation. The Park rows come from a single author, with Protour arrows shot from a compound at 78.9 metres per second through sheets of paper at several distances. Park 2011, using a shooting machine, gives the period of his model, 0.28 seconds with X vanes and 0.25 with Titeflight vanes 24 per cent larger, that is 21.8 and 19.4 metres of flight, and writes that the tears measured in the paper match the calculated ones: that is why his rows say "model and paper test". There the frequency in hertz is our own conversion, one divided by the period, and so carries "≈". Park 2020 finds about 3.7 hertz with the paper, the same value as the model, and warns that the flexing of the shaft makes the measurement approximate. Park's paper tests look at the oscillation in the horizontal plane, not at pitch. Data from: Park 2011, Miyazaki et al. 2017, Ortiz et al. 2018, Ortiz et al. 2020 and Park 2020.
The numbers in the figure
Study or groupValue (oscillations per second (hertz))IntervalnStance
Park 2011, X vanes, model and paper test≈ 3.6for
Park 2011, Titeflight vanes, model and paper test≈ 4for
Miyazaki 2017, Spin Wing, calculation3.95for
Miyazaki 2017, Gas Pro, calculation3.28for
Ortiz 2018, side wind, calculation3.59for
Ortiz 2018, head wind, calculation4.09for
Ortiz 2018, tail wind, calculation3.5for
Ortiz 2020, short straight vanes, calculation4context
Ortiz 2020, large straight vanes, calculation5.3context
Park 2020, paper test≈ 3.7for

The calculations show that the arrow oscillates about its centre of mass after leaving the bow, and since 2011 a measurement has shown it too. The mechanism is always the same: the centre of pressure sits at the back, towards the vanes, the centre of mass sits in front, and as soon as the shaft is tilted against the airflow a moment appears that brings it back into line and makes it swing. Paper tests at several distances on arrows shot from a compound, in 2011 by a shooting machine, find one cycle every nineteen to twenty-two metres and an oscillation that dies away over some twenty-six metres, in line with the same author's model; in simulations of recurve arrows at 57 to 60 metres per second the cycle is fourteen to eighteen metres, and the waviness of the trajectory shows over the first twenty of the seventy metres. The amplitudes are small: in still air the maximum angle stays between a quarter and half a degree, and in the calculation with a three metre per second crosswind it reaches three degrees. The measurements have two limits, though: they come from a single researcher and from a compound, and they look at the oscillation in the horizontal plane rather than in pitch, so for the recurve and in the vertical plane the figures are still model figures.

Also phrased as: "the arrow settles after the first few metres"; "the arrow wobbles in flight"; "arrow porpoising"; "arrow oscillation in flight"; "the arrow groups better far than near"

In practice

Archers say the arrow settles after the first few metres, and use it to explain groups that look worse at short distance than they should.

Evidence

  • 2011
    For Equipment tests Published later

    A model of the arrow as a flexible beam in the horizontal plane, checked against paper tests at several distances on Protour 470 arrows shot from a compound by a shooting machine at 78.9 m/s; the bow was deliberately tuned to exaggerate the lateral oscillation. The arrow oscillates about its centre of mass with a period of about 21.8 m (0.28 s) and a damping time constant of 0.34 s, about 25.8 m of flight; with Titeflight vanes 24% larger the period falls to 19.4 m and the damping increases. The tears measured in the paper match the calculated ones satisfactorily. Paper tests by several compound archers of the Australian national team also agree with the model in both planes, although the author cannot rule out that they were twisting the bow. The oscillation measured with the machine is in yaw rather than pitch, but the mechanism is the same.

    Arrow behaviour in free flight · J L Park

  • 2014
    Context Equipment tests Published later

    In a wind tunnel, on a 2:1 scale model arrow at 30 m/s, the pitching moment stays negative from 0 to 16 degrees of incidence while the lift rises: the arrow tends to realign itself with the airflow, which is the condition for it to oscillate. It measures static stability, not oscillation in flight, and the venue is flagged as questionable.

    Experimental Hydro- and Aerodynamics Research on Arrow Questionable venue · Xiao An Long

  • 2016
    For Model Published later

    An A/C/E arrow with a bullet point and Spin Wing or Gas Pro vanes, fired by compressed air at 60 m/s; the initial attitude comes from four cameras at 3,000 frames per second and the coefficients from a magnetic suspension wind tunnel. In the calculation the angle of attack oscillates and dies away almost entirely in the vertical plane; with ideal launch conditions it stays close to 0 degrees and the air layer stays laminar. In the same work the dynamic test in the tunnel finds the damping term small enough to be neglected. The oscillation is calculated, not measured in flight.

    The boundary layer transition and the attitude of archery allow · Takamasa Matsumoto, Ryu Ando, Takeshi Miyazaki, Satoshi Taguchi, Hiroki Sugiura

  • 2017
    For Model Published later

    Simulation of the flight of an A/C/E arrow launched at 60 m/s, with lift and moment coefficients measured in a magnetic suspension wind tunnel and turbulent drag: the angle of attack oscillates in the vertical plane at 3.95 Hz with Spin Wing vanes and 3.28 Hz with Gas Pro vanes, roughly one cycle every 15 to 18 m, and the amplitude falls by 0.92 and 0.68 per second. The authors note that the frequencies are close to those of the 2011 study and the damping slower, perhaps because the model does not let the shaft flex. The oscillation is calculated.

    Indeterminacy of drag exerted on an arrow in free flight: arrow attitude and laminar-turbulent transition · T Miyazaki, T Matsumoto, R Ando, J Ortiz, H Sugiura

  • 2018
    For Model Published later

    Simulation of the flight of a 14 g A/C/E arrow over 70 m, launched at 57.3 m/s, with coefficients measured in the wind tunnel and in free flight. The angle of attack oscillates at 3.59 Hz with a 3 m/s crosswind, 4.09 Hz with a headwind and 3.50 Hz with a tailwind, and the amplitude falls by 0.87 per second through the effect of the vanes. The waviness of the trajectory is evident over the first 20 m, the first 0.40 s of a flight lasting under 1.3 s, and then fades. With a 3 m/s crosswind the maximum angle reaches 3.0 degrees. The arrow is treated as a rigid body, with no flexing.

    Trajectory and attitude of an archery arrow in free flight:: estimation of the influence of the background wind. · Julio Ortiz, Masato Ando, Takeshi Miyazaki

  • 2019
    For Review Published later

    A narrative review of outdoor target archery. Summarising the author's own free-flight model, it reports that fletched arrows oscillate in pitch or yaw about their centre of mass with a period corresponding to about 20 m travelled, that the calculated period matched the measured one, and that the moment comes mainly from the lift of the vanes, which act on a far longer lever arm than the drag does. It does not report the measurement data.

    The impact of the atmosphere on target archery · James L Park

  • 2020
    Context Equipment tests Published later

    A/C/E 1206 arrows with straight vanes, fired by compressed air over 55 m indoors with a 200 Hz inertial sensor inside the shaft. In a shot at 56.4 m/s, with 1.04 s of flight, the average deceleration is 0.65 G up to 0.40 s and about 0.30 G after 0.45 s, which the authors read as the return to laminar flow once the calculated angle of attack drops below 0.3 degrees, from a maximum of about 0.36. In the calculation the angle oscillates at 4 Hz with the small vanes and 5.3 Hz with the large ones. What is measured is drag, not the oscillation.

    Experimental and Computational Study of Archery Arrows Fletched with Straight Vanes · Julio Ortiz, Atsushi Serino, Toshinari Hasegawa, Takahito Onoguchi, Hiroki Maemukai, Takeshi Miyazaki, Hiroki Sugiura

  • 2020
    For Equipment tests Published later

    In the paper on wind drift the author reports a paper test at several distances with a Protour 380 shot from his compound, which launches that arrow at 78.9 m/s: the measured oscillation has a frequency of about 3.7 Hz, the same as the model, which gives it a damping time of 0.49 s. At that speed this is about 21 m per cycle. The author warns that the flexing of the shaft makes the measurement approximate.

    The dynamic behaviour of an arrow in wind · James L Park

  • 2022
    Context Equipment tests Published later

    Automatic analysis of footage at 3,000 frames per second on A/C/E arrows fired by compressed air at 40 to 60 m/s in a 55 m hall: measured angles of attack under 1 degree and angular velocities under 0.5 rad/s over the filmed stretch. Using those data as a starting point, the calculation gives a maximum angle of attack of 0.46 or 0.51 degrees with a streamlined point and 0.44 with a bullet point. It measures the attitude near the launch, not the oscillation along the flight.

    Automatic image analysis of an archery arrow in free flight using high-speed video cameras · Riku Murakami, Hiroya Mamori, Takeshi Miyazaki, Naoya Takahashi

Status history

  1. 2011 Reported The first data already include a measurement. A model treating the arrow as a flexible beam is checked against paper tests at several distances on Protour 470 arrows shot from a compound by a shooting machine at 78.9 metres per second: the arrow oscillates about its centre of mass with a period of about 21.8 metres, and the oscillation dies away over about 25.8 metres of flight; with vanes 24 per cent larger the period drops to 19.4 metres. The tears in the paper match the calculation. It is a single study, on a compound, and the oscillation measured is the one in the horizontal plane, which follows the same mechanism as pitching: reported.
  2. 2014 Reported A wind tunnel test on a 2:1 scale model arrow finds the pitching moment negative throughout from 0 to 16 degrees of incidence: the arrow tends to realign itself with the airflow, which is the condition for it to oscillate. This is static stability, not oscillation in flight, and the journal is flagged as a questionable venue: the status does not change.
  3. 2016 Reported The first calculation in the vertical plane arrives. Starting from the launch attitude measured with four cameras at 3,000 frames per second, on an A/C/E arrow fired by compressed air at 60 metres per second, the simulation shows an angle of attack that oscillates and dies away, almost entirely in the vertical plane; with a perfect launch the angle stays close to zero. It is the pitching the claim describes, but calculated and without a period: the status stays reported on the strength of the 2011 measurement.
  4. 2017 Reported The same Japanese group puts a figure on the pitching of a recurve arrow. In the simulation at 60 metres per second, with coefficients measured in the wind tunnel, the angle of attack oscillates at 3.95 hertz with Spin Wing vanes and 3.28 with Gas Pro, roughly one cycle every fifteen to eighteen metres, and with the larger vanes it dies away sooner. The authors note that the frequencies are close to those of the 2011 study, while the damping is slower. It is a model, so the status does not change.
  5. 2018 Reported More figures, again from a simulation with parameters taken from the wind tunnel and from free flight. At 57 metres per second the angle of attack oscillates 3.59 times per second in a crosswind, 4.09 in a headwind and 3.50 in a tailwind, roughly one cycle every fourteen to sixteen metres, and the amplitude falls by 0.87 per second thanks to the vanes. The waviness of the trajectory shows mostly over the first twenty of the seventy metres, the first four tenths of a second of a flight lasting under 1.3. It is the picture the claim describes, but calculated: the status does not change.
  6. 2019 Reported A review gives the round figure: fletched arrows oscillate in pitch and yaw about their centre of mass with a period corresponding to about twenty metres travelled, and the calculated period matched the measured one. It is the author of the 2011 measurement summarising his own work, and a review does not decide the status: reported.
  7. 2020 Reported Two papers in the same year. An inertial sensor inside the shaft, on arrows fired by compressed air at 56.4 metres per second over 55 metres indoors, records an average deceleration of 0.65 G over the first four tenths of a second and of about 0.30 G after forty-five hundredths, which the authors read as the airflow turning laminar again once the calculated angle of attack drops below three tenths of a degree: it is consistent with an oscillation dying away over the first stretch, but what it measures is drag. The same year the author of the 2011 tests repeats the paper test at several distances with a Protour 380 from his compound and finds about 3.7 hertz, the frequency of his model, roughly one cycle every twenty-one metres. The direct studies become two, but they come from the same researcher, with the same instrument, on a compound and in the horizontal plane, and the author himself warns that the flexing of the shaft makes the test approximate: that is not enough for corroborated, and the status stays reported.
  8. 2022 Reported Automatic analysis of high-speed footage measures the arrow's attitude over the stretch covered by the cameras: angles of attack under one degree and angular velocities under half a radian per second, and in the calculation built on them a maximum angle of 0.44 to 0.51 degrees. It confirms that the oscillation is small, but measures neither its period nor its damping along the flight: the status stays reported.

Related

Related articles

Research lines

Cite
APA

Campagna, M. (2026). In flight the arrow oscillates in pitch, one cycle every fourteen to twenty-two metres, and the waviness shows mostly over the first stretch (Version 2). In Evidence Registry. Retrieved 16 October 2026, from https://matteocampagna.com/en/registry/equipment/arrow-pitch-oscillation-in-flight

BibTeX
@misc{campagna2026_oscillazionebeccheggiovolo,
  author = {Campagna, Matteo},
  title = {In flight the arrow oscillates in pitch, one cycle every fourteen to twenty-two metres, and the waviness shows mostly over the first stretch},
  year = {2026},
  howpublished = {Evidence Registry, matteocampagna.com},
  url = {https://matteocampagna.com/en/registry/equipment/arrow-pitch-oscillation-in-flight},
  note = {Version 2; accessed 2026-10-16}
}

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