1955•NASA STI Repository (National Aeronautics and Space Administration)Requires access

The Effect of Inlet Installation on the Zero-lift Drag of a 60 Degree Delta-wing--body Configuration from Flight Tests at Mach Numbers from 0.8 to 1.86

Charles F Merlet

Open publisher page 0 citations

Abstract

This record does not include an abstract. Use the full-text link above if available.

About this research paper

What this paper is about

An abstract is not available in the OpenAlex record for this paper.

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.

Key concepts: Mach number, Vortex lift, Lift (data mining), Drag, Wing, Mechanics, Lift-to-drag ratio, Delta wing

Back to paper search Browse research topics Original source

The Effect of Inlet Installation on the Zero-lift Drag of a 60 Degree Delta-wing--body Configuration from Flight Tests at Mach Numbers from 0.8 to 1.86 — Research Paper | ScholarLens