NUST Institutions Library Catalogue catalog › Details for: A practical guide to needs assessment .

Normal view MARC view ISBD view

A practical guide to needs assessment . Catherine M.Sleezer, Darlene Russ-Eft, and Kavita Gupta.

By: Gupta, Kavita, 1958- [author.]Contributor(s): Sleezer, Catherine [author.] | Russ-Eft, Darlene [author.]Material type: Text

TextPublisher: America John Wiley & Sons. 2014Edition: Third EditionDescription: xiv, 402 pages : illustrations ; 23 cmISBN: 9781118457894 (cloth/website)Subject(s): Gupta, Kavita | Training needs -- Evaluation | Needs assessmentAdditional physical formats: Online version:: Practical guide to needs assessment.DDC classification: 658.3124 LOC classification: HF5549.5.T7 | G87 2014

Tags from this library: No tags from this library for this title. Log in to add tags.

Holdings ( 1 )
Title notes ( 2 )
Comments ( 0 )

Item type	Current location	Home library	Collection	Shelving location	Call number	Status	Date due	Barcode	Item holds
Book	Central Library (CL)	Central Library (CL)	NFIC	General Stacks	658.3124 SLE (Browse shelf)	Available		NBS10263

Total holds: 0

Hard Cover.

Includes bibliographical references (pages 379-392) and index.

There are no comments on this title.

to post a comment.

Previous
Back to results
Next

1Constitutive Modelling of Ferrocement Elements
by Jokhio, Gul Ahmed
2Bain-ul-aqwami taluqat aur alam e Islam : 1997 and 1998 ke aham waqait elmi tanazir me
by Affan Saljoq
3Control system design of a guide missile
by Mohammad
4Aerodynamic study and design of a helicopter
by Sabahat Khan
5Fabrication of the CAE Remotely Piloted Vehicle
by Tanveer Shehzad
6Fabrication of wing for CAE man powered aircraft
by Rizwan Pasha; Ejaz Yaqoob, advisor
7fabrication and testing of three dimensional wing project
by Ijaz Noor;
8Installation and analysis of heat pump unit
by Farooq Shahid; Khalid Parvez, advisor
9Dynamic stability analysis of an aircraft through computer programme
by Anwar; Ijaz A Malik, Advisor
10stability of cylindrical shell under different types of loading
by Mohammad Amin;
11Dynamic response of a pitch rate control system for an air to air cruise form guided missile
by Zahid Baig;
12Determination of static stability of an aircraft through wind tunnel tests
by Hafeez
13Effect of winglets on 3D wings
by Mahmood Abdul Jabbar IRAQ A F
14Design of an overlapping wing aircraft
by Jehanzeb Masud
15To verify prandtl gluaert similarity rule
by Nisar Kingravi; Zakir Khan, Advisor
16Design of a turbo jet engine axial flow turbine
by Naeem ud Din
17Design of a turbo jet engine axial flow compressor
by Abdul Hayee
18Study of vibratory behaviour of continuous bodies
by Saleem ur Rehman
19Study of thrust augmentation processes of jet engines
by Ali Nadeem
20Self study of rocket engine performance and evaluation of performance parameters
by Anwar Hasan
21Shakedown analysis of beam and framed structures
by Ehsanullah; Muzzafar Haider, advisor
22To Predict the Off-Design Performance of Axial-Flow Multistage Compressors and to write a computer programme
by Inam-Ul-Haq Raja
23Verification of Theodorson's thick Aerofoil Theory Project
by Noor Abbas
24Structural Design and Fabrication of fuselage of CAE light Aircraft
by Nadeem Jalil
25To verify Prandtl Gluaert Similarity Rule
by SHARAF RABBANI
26Wind Tunnel testing of CAEOverlapping winged Aircraft
by Zaeem Masud
27Redesign of F-6 Wing
by Khurram Rehman
28Design of Axial Flow Compresser
by Ateeque
29Structural Design and Fabrication of Control Surfaces of light Aircraft
by Nasir Maqsood Sulery
30Installation testing and calibration of universal vibration apparatus
by Waleed A Rehman,UO IAF
31Design of Air Combat Fighter XF-23 A Moos
by Rashid Ali Al Saadi
32Foundation wiring and pipe diagrams of compressors dryer unit and storage tank of supersonic wind tunnel along with the layout and packing and transportation procedures of the tunnel
by Jamil Ahmad Qureshi
33Electrical /pressure pipe diagrams of supersonic wind tunnel and its caliberation
by Khurram Bashir
34Transportation of subsonic wind tunnel and the two balance systems
by Ishaat Saboor Khan
35Design & Manufact of Fixtures Measurement of Mirage III A/C Fabrication of Mirage III model to be tested in CAE wind
by Rashid Al Saadi
36caliberation of subsonic wind tunnel
by Jawad A Toor
37Design of jigs and fixtures and disassembly reassembly sequence for shifting of subsonic wind tunnel
by Amjad Mahmud
38Transportation re-installation, calibration and experimentation of MAN torsional testing machine
by Azhar Sajjad
39Aerodynamic analysis of F-6 model aircraft
by Irfan; Shiraz, Advisor
40re-installation, calibration and running of Amsler 10 ton tensile testing machine
by Shafqat Ali Bhatti
41MAN 60 ton universal testing machine
by Umar Qayyum S M
42To study the axial flow compressor by actuator disc theory
by Malik M Rafique; Zaidi SM and khalid parvez, advisors
43Variable area supersonic inlet design
by Rana Zahid F A; Zaidi SKN, advisors
44To study the effect of sweep back wing performance
by Akhlaq A Khan
45Computer simulation of methods of characteristics
by Sohail E James; shiraz aslam, advisor
46Comparison of forward swept and aft swept wing in subsonic regime
by Shahid Hamid; Khalid Khan, advisor
47Design and fabrication of CAE light aircraft wing
by Munir M Baig GC; Ejaz Yaqoob, advisor
48Design of a combustion chamber (inlet)
by Rahman Gul; Khalid Parvez, advisor
49fabrication of wing for CAE man powered aircraft
by Mohammad Munawar Javed; Ejaz Yaqoob, advisor
50Study of ejector nozzle
by Muhammad Afzal;