1952•Unpublished venueRequires access

Longitudinal stability, trim, and drag characteristics of a rocket-propelled model of an airplane configuration having a 45 degree sweptback wing and an unswept horizontal tail

James H Parks, Alan B Kehlet

Abstract

Report discussing an investigation of the longitudinal stability, trim, and drag of a rocket-propelled model at low lift coefficients at a range of Mach numbers. the configuration included a wing and horizontal tail of aspect ratio 4 and thickness ratio in the streamwise direction of 6 percent.

About this research paper

What this paper is about

Why it matters

A significance statement is not available in the OpenAlex record.

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

Key concepts: Trim, Longitudinal static stability, Airplane, Lift-to-drag ratio, Drag, Lift-induced drag, Aerospace engineering, Wing