The rotor wake above a tiltrotor airplane-model in hover

A. Darabi, A. Stalker, M. McVeigh, Israel J Wygnanski

Research output: Chapter in Book/Report/Conference proceedingConference contribution

8 Citations (Scopus)

Abstract

The mean and time-dependent rotor-wake flow over a XV-15 tiltrotor model in hover was studied using stereoscopic particle-image velocimetry. Results from the full-span model were compared to those obtained from a semispan model simulated using an image-plane. Additional data were measured in the wakes of single and twin rotors without the airframe present, with and without an image plane. Rotor wake contraction was considerably reduced over the semi-span model when compared to the full-span case. This is attributed to pressure increases above the fuselage due to the elimination of the lateral flow fluctuations by the solid image plane. In the absence of the image-plane, the correlation between pairs of tip vortices from opposing rotors was negative (i. e. vortices were moving in the same direction) near the centerline of the aircraft. In the absence of the airframe model, the wake flow of two side-by-side rotors was almost indistinguishable from that observed on a single rotor in conjunction with an image plane.

Original languageEnglish (US)
Title of host publication33rd AIAA Fluid Dynamics Conference and Exhibit
StatePublished - 2003
Externally publishedYes
Event33rd AIAA Fluid Dynamics Conference and Exhibit 2003 - Orlando, FL, United States
Duration: Jun 23 2003Jun 26 2003

Other

Other33rd AIAA Fluid Dynamics Conference and Exhibit 2003
CountryUnited States
CityOrlando, FL
Period6/23/036/26/03

Fingerprint

Rotors
Aircraft
Airframes
Vortex flow
Fuselages
Velocity measurement

ASJC Scopus subject areas

  • Fluid Flow and Transfer Processes
  • Energy Engineering and Power Technology
  • Aerospace Engineering
  • Mechanical Engineering

Cite this

Darabi, A., Stalker, A., McVeigh, M., & Wygnanski, I. J. (2003). The rotor wake above a tiltrotor airplane-model in hover. In 33rd AIAA Fluid Dynamics Conference and Exhibit

The rotor wake above a tiltrotor airplane-model in hover. / Darabi, A.; Stalker, A.; McVeigh, M.; Wygnanski, Israel J.

33rd AIAA Fluid Dynamics Conference and Exhibit. 2003.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Darabi, A, Stalker, A, McVeigh, M & Wygnanski, IJ 2003, The rotor wake above a tiltrotor airplane-model in hover. in 33rd AIAA Fluid Dynamics Conference and Exhibit. 33rd AIAA Fluid Dynamics Conference and Exhibit 2003, Orlando, FL, United States, 6/23/03.
Darabi A, Stalker A, McVeigh M, Wygnanski IJ. The rotor wake above a tiltrotor airplane-model in hover. In 33rd AIAA Fluid Dynamics Conference and Exhibit. 2003
Darabi, A. ; Stalker, A. ; McVeigh, M. ; Wygnanski, Israel J. / The rotor wake above a tiltrotor airplane-model in hover. 33rd AIAA Fluid Dynamics Conference and Exhibit. 2003.
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