Ramana ppt

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By: CHENNA VENKATA RAMANA SUPER SONIC AIR CRAFT G. PULLAREDDY ENGINEERING COLLEGE , KURNOOL

Transcript of Ramana ppt

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By:CHENNA VENKATA RAMANA

SUPER SONIC AIR CRAFT

G. PULLAREDDY ENGINEERING COLLEGE , KURNOOL

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Introduction History of Aviation Industry Principle of working Concepts Advantages Disadvantages conclusion

CONTENTS

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The first aircraft to fly supersonically in level flight was the American Bell X-1 experimental plane which was powered by a 6000-lb thrust rocket powered by liquid oxygen and ethyl alcohol.

Introduction

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History of aviation started with Kites Super sonic and Hyper sonic flights were

Introduced (which is too heavier than airjets- unscientific design)

History of Aviation Industry

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17th 18th 19th century Hydrogen Gas is discovered which leads to the invention of Hydrogen balloons.

Physicist- leads to the H-balloons with hot air

20th century- Aerodynamics made by physicist.

Innovations…

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SUPER SONIC AIR CRAFT PRINCIPLE: Flight at speeds greater than that of sound

are supersonic. The range of speeds from Mach number 0.8

to 1.2 is known as transonic

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Supersonic Configuration Concepts

Supersonic laminar flow

Tsagi SSBJ

Lockheed All-Wing

Lockheed low-boom

Oblique wing

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Evolution of Geometry ModelingCircular cross-sectionStraight tapered wing

Elliptic cross-sectionStrake modeled

Axisymmetric nacelles and spikes

Nacelles with 2D inlets

Curved leading edges2D circular nacellesSplit cross-section(different widths above and below wing)

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Large range of concepts requiring flexible, high-fidelity geometry representation

High sensitivity to geometric changes Many sources of non-smooth behavior High dimensionality search space

Supersonic Optimization Challenges

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Multidisciplinary Analysis and Design Methods

Parametric Geometry Viscous and Inviscid Analysis Tools Suite of Search Methods Multiobjective / Multipoint Optimization Multifidelity Search Experiments

Tools for Meeting The Challenges

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Applications of optimization

Basic aero/structural trades with aeroelastic constraints

High-speed lines, inlet/nozzle design, integration

Boom tailoring

Wing/body/nacelle design with transition and total drag estimation

Example Optimization Studies

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 High Speed Quick Service Easy Access: No Physical Barrier: Natural Route: National Defence: No Infrastructure Investment

Advantages

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 Risky: Very Costly: Small Carrying Capacity: Unreliable: Huge Investment

Disadvantages

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Thank You