1976Defense Technical Information Center (DTIC)Requires access

Aerodynamic Characteristics of a Series of Bodies with and without Tails at Mach Numbers from 0.8 to 3.0 and Angles of Attack from 0 to 45 degrees.

Jimmie N. Derrick, D. J. Spring, G. C. Winn

Open publisher page 3 citations

Abstract

Wind tunnel tests were conducted in a 16 ft. transonic tunnel, a supersonic tunnel, A and a trisonic tunnel to establish a bank of systematic data for body and body-tail configurations at high angles of attack. The configurations were tested at Mach numbers between 0.8 and 3.0, angles of attack from -2 to 45 degrees, and roll angles from 0 to 90 degrees. The aerodynamic characteristics were obtained for the total configuration as well as each of the four undeflected tail fins.

About this research paper

What this paper is about

Wind tunnel tests were conducted in a 16 ft. transonic tunnel, a supersonic tunnel, A and a trisonic tunnel to establish a bank of systematic data for body and body-tail configurations at high angles of attack. The configurations were tested at Mach numbers between 0.8 and 3.0, angles of attack from -2 to 45 degrees, and roll angles from 0 to 90 degrees. The aerodynamic characteristics were obtained for the total configuration as well as each of the four undeflected tail fins.

Why it matters

OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

Wind tunnel tests were conducted in a 16 ft. transonic tunnel, a supersonic tunnel, A and a trisonic tunnel to establish a bank of systematic data for body and body-tail configurations at high angles of attack. The configurations were tested at Mach numbers between 0.8 and 3.0, angles of attack from -2 to 45 degrees, and roll angles from 0 to 90 degrees. The aerodynamic characteristics were obtained for the total configuration as well as each of the four undeflected tail fins.

Key concepts: Mach number, Transonic, Supersonic speed, Aerodynamics, Wind tunnel, Supersonic wind tunnel, Angle of attack, Series (stratigraphy)

Related papers

Back to paper searchBrowse research topicsOriginal source
Aerodynamic Characteristics of a Series of Bodies with and without Tails at Mach Numbers from 0.8 to 3.0 and Angles of Attack from 0 to 45 degrees. — Research Paper | ScholarLens