Jove
Visualize
Contact Us
JoVE
x logofacebook logolinkedin logoyoutube logo
ABOUT JoVE
OverviewLeadershipBlogJoVE Help Center
AUTHORS
Publishing ProcessEditorial BoardScope & PoliciesPeer ReviewFAQSubmit
LIBRARIANS
TestimonialsSubscriptionsAccessResourcesLibrary Advisory BoardFAQ
RESEARCH
JoVE JournalMethods CollectionsJoVE Encyclopedia of ExperimentsArchive
EDUCATION
JoVE CoreJoVE BusinessJoVE Science EducationJoVE Lab ManualFaculty Resource CenterFaculty Site
Terms & Conditions of Use
Privacy Policy
Policies

Related Concept Videos

Typical Model Studies01:30

Typical Model Studies

376
Fluid mechanics model studies often utilize scaled-down systems to predict fluid behavior in full-scale environments, such as river flows, dam spillways, and structures interacting with open surfaces. Maintaining Froude number similarity in river models is crucial, as it replicates surface flow features like wave patterns and velocities.
376
Lift01:23

Lift

180
Lift is a fundamental aerodynamic force that acts perpendicular to the direction of airflow. It plays a central role in achieving and sustaining flight and in stabilizing various vehicles. Lift primarily originates from pressure differences created across surfaces, such as an airfoil. A lower pressure region forms above the wing, while a higher pressure region forms below it, generating an upward force. This differential results from the shape and orientation of the airfoil, enabling the wing...
180
Bernoulli's Equation for Flow Normal to a Streamline01:16

Bernoulli's Equation for Flow Normal to a Streamline

892
Bernoulli's equation for flow normal to a streamline explains how pressure varies across curved streamlines due to the outward centrifugal forces induced by the fluid's curvature. The pressure is higher on the inner side of the curve, near the center of curvature, and decreases outward to balance these centrifugal forces.
The pressure difference depends on the fluid's velocity and radius of curvature. The pressure variation is minimal in flows with nearly straight streamlines.
892
Bernoulli's Equation for Flow Along a Streamline01:30

Bernoulli's Equation for Flow Along a Streamline

1.0K
Bernoulli's equation relates the energy conservation in a fluid moving along a streamline. The equation applies to incompressible and inviscid fluids under steady flow. For such a flow, Newton's second law is applied to a small fluid element, which experiences forces due to pressure differences, gravity, and velocity variations. The force balance leads to the following form of Bernoulli's equation:
1.0K
Design Example: Creating a Hydraulic Model of a Dam Spillway01:21

Design Example: Creating a Hydraulic Model of a Dam Spillway

209
Scaled hydraulic models of dam spillways provide a practical way to replicate and study the intricate flow dynamics of these structures. Often built to a 1:15 ratio, these models allow for observing critical water behavior, such as velocity distribution, flow patterns, and energy dissipation.
209
Turbulent Flow01:24

Turbulent Flow

212
Turbulent flow is characterized by unpredictable fluctuations in velocity and pressure, which result in a chaotic fluid movement distinct from the orderly patterns of laminar flow. While laminar flow is governed by smooth, parallel layers with minimal mixing, turbulent flow exhibits highly irregular, three-dimensional patterns. This behavior arises due to instabilities in the fluid's velocity profile, and amplifies as the flow velocity increases. Minor disturbances, known as turbulent...
212

You might also read

Related Articles

Articles linked to this work by shared authors, journal, and citation graph.

Sort by
Same author

Wind Energy Harvesting with Vertically Aligned Piezoelectric Inverted Flags.

Sensors (Basel, Switzerland)·2023
Same author

Capturing wake capture: a 2D numerical investigation into wing-wake interaction aerodynamics.

Bioinspiration & biomimetics·2022
Same author

Dynamic experimental rigs for investigation of insect wing aerodynamics.

Journal of the Royal Society, Interface·2022
Same author

Wing Planform Effect on the Aerodynamics of Insect Wings.

Insects·2022
Same author

Scalability of resonant motor-driven flapping wing propulsion systems.

Royal Society open science·2021
Same author

The role of the leading edge vortex in lift augmentation of steadily revolving wings: a change in perspective.

Journal of the Royal Society, Interface·2017

Related Experiment Video

Updated: Jul 15, 2025

Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods
09:17

Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods

Published on: April 23, 2018

10.8K

A simple model of wake capture aerodynamics.

Mostafa R A Nabawy1,2

  • 1School of Engineering, The University of Manchester, Manchester M13 9PL, UK.

Journal of the Royal Society, Interface
|September 26, 2023
PubMed
Summary

This study models how flapping wings capture previous wake effects, improving aerodynamic force predictions for insect flight. Results show high wing speeds near stroke reversal significantly increase wake capture forces.

Keywords:
aerodynamicsanalytical modellingflapping wingsinsect flightwake capturewing–wake interaction

More Related Videos

A Rapid Method for Modeling a Variable Cycle Engine
04:58

A Rapid Method for Modeling a Variable Cycle Engine

Published on: August 13, 2019

7.6K
A Microfluidic Model of Biomimetically Breathing Pulmonary Acinar Airways
09:39

A Microfluidic Model of Biomimetically Breathing Pulmonary Acinar Airways

Published on: May 9, 2016

8.0K

Related Experiment Videos

Last Updated: Jul 15, 2025

Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods
09:17

Experimental Investigation of the Flow Structure over a Delta Wing Via Flow Visualization Methods

Published on: April 23, 2018

10.8K
A Rapid Method for Modeling a Variable Cycle Engine
04:58

A Rapid Method for Modeling a Variable Cycle Engine

Published on: August 13, 2019

7.6K
A Microfluidic Model of Biomimetically Breathing Pulmonary Acinar Airways
09:39

A Microfluidic Model of Biomimetically Breathing Pulmonary Acinar Airways

Published on: May 9, 2016

8.0K

Area of Science:

  • Aerodynamics
  • Bio-inspired engineering
  • Fluid mechanics

Background:

  • Flapping wings interact with their own wake, influencing aerodynamic forces.
  • Existing quasi-steady models for insect flight often neglect these wake capture effects.

Purpose of the Study:

  • To develop a simple method for incorporating wake capture effects into analytical quasi-steady models.
  • To improve the prediction of aerodynamic forces in hovering insect flight.

Main Methods:

  • Modeled the local wake flow field as an additional induced velocity component.
  • Integrated this component into existing quasi-steady models, switching it in at each half-stroke.
  • Compared model predictions with experimental data for eight test cases.

Main Results:

  • The model showed satisfactory agreement with experimental data for lift and drag variations.
  • Sensitivity analysis revealed that the wing's translational velocity profile significantly impacts wake capture forces.
  • High translational velocity profiles up to stroke reversal resulted in larger wake capture effects compared to sinusoidal profiles.

Conclusions:

  • The developed approach effectively predicts wake capture effects in insect flight.
  • Translational velocity profiles significantly influence aerodynamic forces, with implications for natural and engineered flapping flight.
  • High accelerations near stroke reversal, while enhancing wake capture, are mechanically costly and impractical.