Extreme Range Breguet Range eq. best values based on current technology:   p = 0.9  c p = 0.4 (piston engine gives the best sfc)  L/D = f (A, e, C.

Slides:

Advertisements

Similar presentations

How Airplanes Fly Forces

Advertisements

By Anthony, Reuben and Micheal

Airplanes 1 Airplanes. Airplanes 2 Introductory Question As you ride in a jet airplane, the clouds are passing you at 600 mph. The air just in front of.

Presented by Dan Shafer James Pembridge Mike Reilly

AE 1350 LECTURE #3 TOPICS PREVIOUSLY COVERED Roadmap of Disciplines “English” to “S.I.” units Common Aerospace Terminology Airplane Axes and Motion This.

Principles of Aviation

DR2 Aerodynamic PDR II Aerodynamic Preliminary Design Review II “The 20 Hour Marathon” October 19, 2000 Presented By: Loren Garrison Team DR2 Chris Curtis.

Vertical Launch UAV Project Plan. ∞ Construct an unmanned aerial vehicle (UAV) with a camera payload ∞ UAV must autonomously navigate with real-time video.

Guidelines Presentation. Aircraft Aim & Judging The aircraft needs to transport the mirror segments of the ESO European Extremely Large Telescope, being.

Oklahoma Space Grant Long Range/Endurance UAV projects.

Bernoulli's Principle It explains why and airplane gets lift

AE 10 Airplane Design. Preliminary Aircraft Design Process 1. Mission Specification 2. Configuration Design 3. Weight Sizing 4. Performance Sizing 5.

MAE 1202: AEROSPACE PRACTICUM Lecture 12: Swept Wings and Course Recap April 22, 2013 Mechanical and Aerospace Engineering Department Florida Institute.

U5AEA15 AIRCRAFT STRUCTURES-II PREPARED BY Mr.S.Karthikeyan DEPARTMENT OF AERONAUTICALENGINEERING ASSISTANT PROFESSOR.

Lesson 28 Cruise Range and Endurance

AAE 451 Aircraft Design Aerodynamic Preliminary Design Review #1

Click to edit Master title style Click to edit Master text styles Second level Third level Fourth level Fifth level 1.

Click to edit Master title style Click to edit Master text styles Second level Third level Fourth level Fifth level 1.

Wing Planform Optimization via an Adjoint Method

Aero Engineering 315 Lesson 33 GR3 Review. General strategy  Prior to class Review reading for lessons 23 – 32 Work / review problems #26 – 42 Review.

MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS

UAV UF 118 Night Falcon ONE OF THE ULTIMATE DEFENSE SYSTEMS FROM SURVAILLANCE TO TAKING OUT ANYTHING THAT MOVES.

MAE 4261: AIR-BREATHING ENGINES

The Four Forces of Flight

Joining of Different Type “Wing-Body” Surfaces of Aircraft Structure

 Flight deck  Engines  CO2, noise and fuel consuption  Materials  Wings  Cabins.

Virginia Tech Truss-Braced Wing Studies

MAE 1202: AEROSPACE PRACTICUM Introduction to Aircraft Performance: Part 2 April 7, 2008 Mechanical and Aerospace Engineering Department Florida Institute.

AE 1350 Lecture Notes #9.

PROPRIETARY James Bearman AJ Brinker Dean Bryson Brian Gershkoff Kuo Guo Joseph Henrich Aaron Smith Daedalus Aviation Conceptual Design Review: “The Daedalus.

Theory of Flight 6.05 Lift and Drag

Design Chapter 8 First Half. Design Requirements and Specifications Payload Range Cruising Speed Takeoff & Landing Distance Ceiling.

DESIGN OF THE 1903 WRIGHT FLYER REPLICA MADRAS INSTITUE OF TECHNOLOGY CHENNAI - 44.

1. Mission Statement Design Requirements Aircraft Concept Selection Advanced Technologies / Concepts Engine / Propulsion Modeling Constraint Analysis.

By: Ava and Audrey. Thrust Thrust is forward motion. The airplane’s engine’s produce thrust. It is one of the forces that the airplane needs to fly. It.

Basic Aeronautics Know the principles of basic aeronautics. 1. Describe the effects of angle of attack. 2. Identify the four forces of flight.

AAE 451 Aircraft Design First Flight Boiler Xpress November 21, 2000

AVIATION HISTORY Lecture 8: Speeds of Flight. Introduction  After the invention of the airplane, designers and engineers created new aircraft for a variety.

Compound Aircraft Transport 1) Mx – 1018 project B-29/F-84 2) Tom-Tom Project B-36F/F-84 Model Problems of Compound Flight Configuration IConfiguration.

AE1202 ELEMENTS OF AERONAUTICS Semester III AERONAUTICAL ENGINEERING Handled by K.PADMANABAN.

Basic Aeronautics Know the principles of basic aeronautics. 1. Describe the effects of angle of attack. 2. Identify the four forces of flight. Lesson.

Chalmers University of Technology Elementary axial turbine theory –Velocity triangles –Degree of reaction –Blade loading coefficient, flow coefficient.

DR2 Aerodynamic PDR Aerodynamic Preliminary Design Review October 3, 2000 German National Holiday Presented By: Loren Garrison Team DR2 Chris Curtis Chris.

Airfoil Selection and Tail Design Jose Pedrego ASCEND Team 4/19/2008.

Modern Design Concept Chapter 10. Aerodynamic Research Contributions Propulsion Structural Design Monocoque structure Optimum location for the engine.

AE 2350 Lecture Notes #9 May 10, 1999 We have looked at.. Airfoil aerodynamics (Chapter 8) Sources of Drag (Chapter 8, 11 and 12) –Look at the figures.

The problems with early Flight By Jared DaSilva- G&T: Aviation.

LSA FAA definition Max gross takeoff weight = 1320 lbs Max stall speed = 45 knots Maximum speed in level flight = 120 knots.

Brian Acker Lance Henricks Matthew Kayser Kevin Lobo Robert Paladino Ruan Trouw Dennis Wilde.

Zuliana-July Lecture 1: INTRODUCTION AIRCRAFT MASS (WEIGHT) & PERFORMANCE By: Zuliana Ismail, 2010.

? ?? ? Imagine if… There were no airplanes… What would we need to fly???

12/11/12 Brandon Campbell & Ernesto Chairez. Purpose  Civil Transport  Large Volume  Efficient  Quiet  Long Range.

AVIATION HISTORY Lecture 8: Speeds of Flight. Introduction  After the invention of the airplane, designers and engineers created new aircraft for a variety.

CASE STUDY ON “AVIATION” BY VISHAL DESHPANDE VINAY AKKI SHABAZ BHAVIKATTI SHAHASAN NOUSHAD Slide 1.

SAE Aero 2017 Midterm Presentation Joe Zongolowicz, Nick Montana, Frank Dixon, Kevin Scheventer, Kathy Hansen, Marquis Ward, Gerald Short, Zhangsiwen Xiao,

Team “Canard” September 28th, 2006

Presentation on Optical Computing

Aircraft and its parts prap.Radek Heryan

Airplane Parts and Theory of Flight

Matching of Propulsion Systems for an Aircraft

FLIGHT MECHANICS BDA DR. ZAMRI BIN OMAR D

Civil jet aircraft performance

The lifting power of air

Aether Aerospace AAE 451 September 27, 2006

Model Problems of Compound Flight

Boom Supersonic 11/11/17 Agenda

Types of aircraft Revision CPL František Vlasák.

Vocabulary in your own words

Air, Aerodynamics, and Flight

Presentation transcript:

Extreme Range Breguet Range eq. best values based on current technology:   p = 0.9  c p = 0.4 (piston engine gives the best sfc)  L/D = f (A, e, C D0 )  C D0 = f (S wetted, BL state, S)

Extreme Range  Structural limits to max allowable A  Aerodynamic limits to C D0  Powered airplanes: (L/D) max = 25 very good value !  Transports W i / W f = 2.0  R max = 14,621 n. mi.  Nonstop, unrefueled flight around the world R = 28,000 n.mi. ! This range requires a W i / W f = 3.8  Nothing you can do in a short time to overcome technology limitations! The only thing you can do is be creative in your design!

Extreme Range Rutan achieved W i / W f = 4.5 in the Voyager with:  A = 33.8  Composites  Special airfoils in the lifting surfaces and the propellers  Place fuel outboard on the wing:  Reduce wing root bending moment  Improve W i / W f  Experimental regulations instead of civil or military airworthiness constraints, resulting in W savings

Rutan Voyager

Extreme Endurance Breguet Endurance eq. Same tradeoff between L / D and W as in the case of extreme range

Extreme L / D High-performance gliders: Schleicher AS W22 B

Extreme L / D Need to maximize A and minimize C D0 Solutions:  Very high A wings (Schleicher AS W22 has A = 38.3)  Laminar flow wings  Min size fuselage (pilot in reclined position)  Advanced composite structures