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    PARK COLLEGE OF TECHNOLOGYDEPARTMENT OF MECHANICAL ENGINEERING

    LESSON PLAN

    SUBJECT CODE ME2351

    SUBJECT NAME GAS DYNAMICS AND JET PROPULSION

    CLASS/SEM III MECH/VI SEM

    STAFF INCHARGE M.SATHEESH KUMAR

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    SYLLABUS (REGULATION 200! AU CHENNAI"

    UNIT I # BASIC CONCEPTS AND ISENTROPIC FLO$S %Energy and momentum equations of compressible uid ows Stagnation states, Machwaves and Mach cone Eect of Mach number on compressibility Isentropic ow throughvariable ducts o!!le and "iusers #se of $as tables%

    UNIT II # FLO$ THROUGH DUCTS &&lows through constant area ducts with heat transfer '(ayleigh ow) and &riction '&annoow) variation of ow properties #se of tables and charts $enerali!ed gas dynamics%

    UNIT III # NORMAL AND OBLI'UE SHOCKS10

    $overning equations *ariation of ow parameters across the normal and oblique shoc+s randtl Meyer relations #se of table and charts -pplications%

    UNIT IV # JET PROPULSION10

    .heory of /et propulsion .hrust equation .hrust power and propulsive e0ciency 1peration principle, cycle analysis and use of stagnation state performance of ram /et,turbo/et, turbofan and turbo prop engines%

    UNIT V # SPACE PROPULSION10

    .ypes of roc+et engines ropellants2feeding systems Ignition and combustion .heory ofroc+et propulsion erformance study Staging .erminal and characteristic velocity -pplications space ights%

    TUTORIALS 15! TOTAL %0 PERIODS

    TE)T BOOKS3% -nderson, 4%"%, Modern 5ompressible ow, Mc$raw 6ill, 7 rd Edition, 8997%8% 6% 5ohen, $%E%5% (ogers and Saravanamutto, $as .urbine .heory, :ongman $roup :td%,3;

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    UNIT NO

    PROPOSED

    DATE OF

    COMPLETIO

    N

    TOPICS TO BE COVEREDNO. OF

    HOURS

    TEACHIN

    G AIDS

    I2-SI5

    515E.S

    -"ISE.(1I5

    &:1?

    3% Energy and momentum

    equations of compressible

    uid ows 7

    oardF

    5hal+

    8% Stagnation states 8

    7% Mach waves and Mach cone 3

    D% Eect of Mach number on

    compressibility8

    C% Isentropic ow through

    variable ducts o!!le and

    "iusers

    B

    TOTAL HOURS 15

    II2&:1?

    .6(1#$6

    "#5.S

    3% &lows through constant areaducts with heat transfer

    '(ayleigh ow)

    C

    oardF

    5hal+

    8% &lows through constant areaducts with &riction '&anno

    ow)C

    7% *ariation of ow properties #se of tables and charts 8

    D% $enerali!ed gas dynamics 3

    TOTAL HOURS 13

    III21(M-:

    -"

    1:IG#E

    S615H

    3% $overning equations DoardF

    5hal+8% *ariation of ow parameters

    across the normal and obliqueshoc+s

    D

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    7% randtl2Meyer relations #seof table and charts

    7

    D% -pplications% 3

    TOTAL HOURS12

    UNIT NO

    PROPOSED

    DATE OF

    COMPLETIO

    N

    TOPICS TO BE COVEREDNO. OF

    HOURS

    TEACHIN

    G AIDS

    I*2 4E.(1#:SI1

    3% .heory of /et propulsion 8 .

    8% .hrust equation7

    oardF

    5hal+

    7% .hrust power and propulsivee0ciency 8

    oardF

    5hal+

    D% 1peration principle, cycleanalysis and use of stagnationstate performance of ram /et,turbo/et, turbofan and turbo

    prop engines%

    7.F

    oard

    TOTAL HOURS 10

    *2 (15HE.

    (1#:SI1

    3% .ypes of roc+et engines 3.F

    oard

    8% ropellants2feeding systems 3.F

    oard

    7% Ignition and combustion8

    .F

    oard

    D% .heory of roc+et propulsion 8.F

    oard

    C% erformance study Staging .erminal and characteristic

    velocity

    7oardF

    5hal+

    >% -pplications space ights% 3.F

    oard

    TOTAL HOURS 10

    TOTAL NO.OF HOURS%0

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