ScholarLens Back to search
1965•NASA Technical Reports Server (NASA)Open access

MAXIMUM LIFT-DRAG RATIOS OF DELTA-WING-HALF-CONE COMBINATIONS AT A MACH NUMBER OF 20 IN HELIUM

Patrick Johnston, C. D. Snyder, R. D. Witcofski

Open full text 5 citations

Abstract

Maximum lift-drag ratios of delta wing half-cone combinations in hypersonic helium wind tunnel to determine interference lift

Open-access reader

About this research paper

What this paper is about

Maximum lift-drag ratios of delta wing half-cone combinations in hypersonic helium wind tunnel to determine interference lift

Why it matters

OpenAlex reports 5 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

Maximum lift-drag ratios of delta wing half-cone combinations in hypersonic helium wind tunnel to determine interference lift

Key concepts: Drag divergence Mach number, Mach number, Drag, Lift-induced drag, Physics, Lift-to-drag ratio, Vortex lift, Mechanics

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
MAXIMUM LIFT-DRAG RATIOS OF DELTA-WING-HALF-CONE COMBINATIONS AT A MACH NUMBER OF 20 IN HELIUM — Research Paper | ScholarLens