(PDF) Natural Laminar Flow Nose for Supersonic Transport

Natural Laminar Flow Nose for Supersonic Transport Designed Using Local Non-Axisymmetric Deformation

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN

doi 10.2322/tastj.12.71

Full Text

Abstract

Available in full text

Date

January 1, 2014

Authors

Hiroaki ISHIKAWA

Publisher

Japan Society for Aeronautical and Space Sciences

Related search

Theory of Laminar Viscous-Inviscid Interactions in Supersonic Flow

Aerospace Engineering

English

Natural-Laminar-Flow Airfoil for General-Aviation Applications

Journal of Aircraft

Aerospace Engineering

English

Computed Tomographic Density Measurement of Supersonic Flow Field Around Axisymmetric Model

Transaction of the Visualization Society of Japan

English

Possible Similarity Solutions of the Laminar Natural Convection Flow of Non-Newtonian Fluids

International Journal of Heat and Mass Transfer

Transfer Processes

Condensed Matter Physics

Mechanical Engineering

English

Physical Modeling of Supersonic Flow Over Bodies With Plane and Axisymmetric Shape

MATEC Web of Conferences

Materials Science

English

Prediction of Mass Flow Rate in Supersonic Natural Gas Processing

Oil and Gas Science and Technology

Fuel Technology

Power Technology

Chemical Engineering

Energy Engineering

English

Numerical Study of Flow Angles and Mach Number Measurement Using the Surface Pressure of a Supersonic Aircraft With Nose Cone

Transactions of the Japan Society for Aeronautical and Space Sciences

Planetary Science

Aerospace Engineering

English

Laminar Flow Through Fractal Porous Materials: The Fractional-Order Transport Equation

Communications in Nonlinear Science and Numerical Simulation

Applied Mathematics

Numerical Analysis

English

To the Analysis of the Natural Pulsation Development During Laminar-Turbulent Transition in Supersonic Boundary Layer

English