Numerical Solutions for Axisymmetric Bodies of Revolution in Pitching Oscilliatory Motion Dept. of Power Mechanical Engineering, National Tsing Hua University Taiwan, R.O.C

Format:

Conference/Event

Author/Creator:

Lin, M. H., author.

Conference Name:

Aerospace Technology Conference & Exposition (1990-10-01 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1990

Summary:

A numerical method is developed to analyse the flow around an axisymmetric ogive-cylinder and an ellipsoid-cylinder bodies undergoing harmonic pitching motion in an uniform air free stream. The pressure distributions along the lengthwise and over the circumference of the body are calculated with fineness ratio of 3:1 at mean angle of incidence 0° and 5°. Results are presented for a range of frequency parameters and various mean angle of incidence in order to show the influence of the frequency parameter and the mean angle of incidence on the aerodynamic properties

Notes:

Vendor supplied data

Publisher Number:

901811

Access Restriction:

Restricted for use by site license