This listing was ended by the seller because the item is no longer available.
This is a private listing. Sign in to view your status or learn more about private listings.

 
Posts to:
Australia
Delivery:
Visit store:
Oodals Store
 
Posts to:
Australia

Details about  Jet, Rocket, Nuclear, Ion and Electric Propulsion 9783642461118, Paperback, NEW

Jet, Rocket, Nuclear, Ion and Electric Propulsion 9783642461118, Paperback, NEW See original listing
Jet-Rocket-Nuclear-Ion-and-Electric-Propulsion-9783642461118-Paperback-NEW
Item Ended
Item condition:
Brand new
Ended:
11 Jun, 2014 09:25:50 AEST
Price:
AU $178.54
Postage:
FREE Standard delivery from outside AU | See details
Item location:
Norwich, United Kingdom

Description

eBay item number:
191126809138
Seller assumes all responsibility for this listing.
Last updated on  05 May, 2014 23:30:52 AEST  View all revisions

Item specifics

Condition:
Brand new: A new, unread, unused book in perfect condition with no missing or damaged pages. See the seller's ... Read moreabout the condition
Publisher:

Springer-Verlag Berlin and Heidelberg GmbH & Co. KG

Format:

Softcover

ISBN-10:

3642461115

Language:

English

ISBN-13:

9783642461118

ISBN:

9783642461118

Detailed item info

Key Features
Author(s)W.H.T. Loh
PublisherSpringer-Verlag Berlin and Heidelberg GmbH & Co. KG
Date of Publication08/03/2012
LanguageEnglish
FormatPaperback
ISBN-103642461115
ISBN-139783642461118
SubjectPhysics
Series TitleApplied Physics and Engineering
Series Part/Volume Number7

Publication Data
Place of PublicationBerlin
Country of PublicationGermany
ImprintSpringer-Verlag Berlin and Heidelberg GmbH & Co. K
Content Notebiography

Dimensions
Weight1170 g
Width156 mm
Height234 mm
Spine39 mm

Credits
Edited byW.H.T. Loh

Editorial Details
Format DetailsTrade paperback (US)
Edition StatementSoftcover reprint of the original 1st ed. 1968

Description
Table Of ContentsOne - Introduction.- 1. Fundamentals of Thermodynamics and Aerodynamics.- [1-1] Introduction.- [1-2] Equation of State.- [1-2.1] Equation of State of Real Gases.- [1-3] First Law of Thermodynamics.- [1-3.1] Specific Heats.- [1-3.2] Internal Energy.- [1-3.3] Relationship Between Specific Heats cp and cv.- [1-3.4] Enthalpy.- [1-3.5] Entropy.- [1-3.5.1] Reversible Process.- [1-3.5.2] Adiabatic Process.- [1-3.5.3] Isentropic Process.- [1-3.5.4] Polytropic Process.- [1-3.5.4.1] Work Done.- [1-3.5.4.1.1] Special Case for Isentropic Case where n = k.- [1-3.5.4.1.2] Heat Added.- [1-3.6] Mixture of Gases.- [1-3.7] Entropy-Enthalpy Diagram.- [1-3.7.1] Remarks on Entropy-Enthalpy Diagram.- [1-3.8] The Ideal (Reversible) Cycles.- [1-3.9] Cycle Work, Cycle Heat Added, and Cycle Efficiency.- [1-4] Steady Flow Energy Equation.- [1-4.1] Stagnation Enthalpy or Total Enthalpy, H.- [1-4.2] Application of Steady Flow Energy Equation to Compressor and Turbine Analysis.- [1-5] One-Dimensional Steady Flow Analysis.- [1-5.1] One-Dimensional Energy Equation.- [1-5.2] One-Dimensional Continuity Equation.- [1-5.3] One-Dimensional Momentum Equation without Fluid Shearing or Friction Losses.- [1-5.3.1] One-Dimensional Momentum Equation with Fluid Shearing or Friction Losses.- [1-5.4] Speed of Sound.- [1-5.5] Mach Number.- [1-5.6] Another Form of Energy Equation.- [1-5.7] Isentropic Flow Equations.- [1-6] Normal Shock Waves and Rayleigh and Fanno Lines.- [1-7] Oblique Shock Waves.- [1-8] One-Dimensional Convergent - Divergent Nozzle Flow.- [1-8.1] Nozzle Efficiency.- [1-8.2] Nozzle Thrust.- [1-9] Supersonic Inlet.- [1-9.1] Constant Geometry Supersonic Inlet.- [1-9.2] Variable-Geometry Supersonic Inlet.- [1-9.3] Inlet Diffuser Efficiency.- [1-10] One-Dimensional Flow Analysis with Area Change, Friction and Heat Addition.- [1-10.1] One-Dimensional Flow Analysis with Area Change, Friction and Heat Addition (Additional Analysis).- [1-10.2] Mixing of Two Flows in a Non-Constant Area Duct.- [1-11] Thermodynamic Cycle Analysis.- [1-11.1] Ram Compression and Ram Pressure Recovery.- [1-11.2] Compressor Compression and Compressor Work.- [1-11.3] Combustion and Burner Efficiency.- [1-11.3.1] Combustion.- [1-11.4] Turbine Expansion and Turbine Work.- [1-11.5] Nozzle Expansion and Nozzle Efficiency.- [1-12] Variations of Basic Gas Turbine or Jet Engine Cycles.- [1-12.1] Intercooling.- [1-12.2] Reheat.- [1-12.3] Regeneration.- [1-12.4] After-burning.- [1-12.5] Water Injection.- [1-12.6] Pressure Loss in Various Components.- [1-13.1] Output, Input and Thermal Efficiency.- [1-13.2] Jet Thrust.- [1-13.3] Propeller Thrust.- [1-13.4] Specific Fuel Consumption.- [1-14] Variations of Gas Turbine Cycle and Turbojet Cycle by Gas Table Method.- [1-14.1] Gas Table.- [1-14.2] Example 1: Gas Turbine Analysis.- [1-14.3] Example 2: Turbojet Analysis.- Two - Jet Propulsion.- 2. Thermodynamic Cycle Analysis of Gas Turbines and Air-breathing Propulsion Systems.- [2-1] Introduction.- [2-2] Symbols and Sketches of Air-breathing Propulsion Systems.- [2-3] Gas Turbine Cycles.- [2-4] Air-breathing Propulsion Systems: Turbojet, Turboprop, Ducted Fan, Ram Jet and Ducted Rocket.- [2-4.1] Turbojet Cycles.- [2-4.2] Turboprop Cycles.- [2-4.3] Ducted Fan Cycles.- [2-4.4] Off-Design Point Engines.- [2-4.4.1] Compression Rate Variation with Altitude and Air Speed (Variation with Compressor Inlet Temperature) at Constant Compressor Speed.- [2-4.4.2] Air Flow Variation with Altitude and Airplane Speed at Constant Compressor Speed.- [2-5] Rotary Matrix Regenerator for Turboprop Applications.- [2-5.1] Discussion.- [2-5.2] Operating Principles.- [2-5.3] Theory and Design.- [2-6] Analytical Solutions for Rotary Matrix, Wire Screen Heat Exchangers.- [2-7] Pulse Jet.- [2-7.1] Discharging from Point c to Point a.- [2-7.1.1] Supercritical Discharging When (P/p ? [(k + 1)/2] k/(k ? 1).- [2-7.1.2] Subcritical Discharging When (P/p ? [(k + 1)/2] k/(k? 1).- [2-7.2] Combustion from Point b to Point c.- [2-7.3] Charg

Copyright in bibliographic data and cover images is held by Nielsen Book Services Limited or by the publishers or by their respective licensors: all rights reserved.

Jet, Rocket, Nuclear, Ion and Electric Propulsion 9783642461118, Paperback, BRAND NEW FREE P&H

Jet, Rocket, Nuclear, Ion and Electric Propulsion 9783642461118 W.H.T. Loh oodals

Questions and answers about this item

No questions or answers have been posted about this item.




Place bid

Time left:
Current bid:
(Approximately ##1##)
Shipping:
Import charges:
Your max bid:
Your max bid:
By clicking Confirm bid, you commit to buy this item from the seller if you're the winning bidder.
By clicking Confirm bid, you are committing to buy this item from the seller if you are the winning bidder and have read and agreed to the Global Shipping Program terms and conditions - opens in a new window or tab. Import charges previously quoted are subject to change if you increase you maximum bid amount.
Cancel
Loading...
Resume bidding, if the page does not update immediately.
Place bid
Review and confirm your bid
Bid confirmation
d
h
m
s
day
hour
hours
FREE postage
See item description
(Approximately ##1##)
(Enter ##1## or more)
(Enter more than ##1##)
Your max bid:
Increase max bid
Place bid
Confirm bid
Increase max bid
Cancel
Change bid
Close
, you've been outbid. Don't let it get away - bid again!
, you're the highest bidder on this item. Good luck
, you're the first bidder. Hope you win!
, you're currently the high bidder, but you're close to getting outbid.
, this auction is almost over and you're currently the high bidder.
, you're the high bidder, but the reserve price hasn't been met.
Please enter your bid again.
Please enter a valid number as the bid price.
Enter an amount that is equal or greater than the minimum bid required. This can be found under the bid entry box.
Maximum bids can't be lowered once they're submitted.
This seller requires the buyer to have a PayPal account to purchase this item. Get a PayPal account here .
Your bid is greater than or equal to the Buy It Now price. We recommend you purchase this item via Buy It Now. If you still wish to bid, you may do so below.
Time left:
Current bid:
(approximately ##1##)
Your maximum bid:
(approximately ##1##)
Increase your maximum bid:
By clicking 1 Click Bid, you commit to buy this item from the seller if you're the winning bidder. Learn moreabout 1-click bid - opens in a new window or tab
day
hour
min
sec
days
hours
mins
secs
(approximately ##1##)
Winning bid:
Starting bid:
Close
Congratulations! The auction has ended and you're the winner.
The auction has ended, but the reserve price was not met.
Sorry, the auction has ended and you were outbid.
Good news, you're the high bidder.
Sorry, you've been outbid.
You're the high bidder, but the reserve price is not met.
Please enter a higher amount than the current bid.
Maximum bids can't be lowered once submitted.
Please enter a valid number.
This is a private listing and your identity will not be disclosed to anyone except the seller.

Additional site navigation