یہ ،مجموعہ جولائی 1936 ء میں شائع ہوا۔ بال جبریل کی اشاعت کے ایک ہی سال بعد اردو کلام کا بہت سا حصہ جمع ہو گیا۔ بیماری کے باوجود شعر کے نزول کی کیفیت جاری رہتی ۔ اس کتاب میں بہت سے موضوعات ہیں۔ 183 عنوانات پر مشتمل اس مجموعہ کلام میں علیحدہ کوئی غزل نہیں ہے بلکہ درمیان میں ہی پانچ غزلیات کا عنوان دیا گیا ہے۔ کوئی طویل نظم نہیں ہے۔ بلکہ ”محراب گل افغان کے افکار“ کا عنوان دے کر 20 افکار پیش کیے گئے ہیں۔ افکار کے علاوہ پانچ موضوعات کو مرکزی حیثیت دی گئی ہے۔ (۱) اسلام اور مسلمان (۲) تعلیم و تربیت (۳) عورت (۴) ادبیات ، فنون لطیفہ اور (۵) سیاسیات مشرق و مغرب۔ سرورق پر لکھا ہے۔ ضرب کلیم یعنی ” اعلان جنگ دور حاضر کے خلاف۔ اقبال نے اپنی کتاب کے موضوع کی وضاحت کے لیے سرورق پر کبھی کچھ نہیں لکھا۔ رفیع الدین ہاشمی
لکھتے ہیں:
”یہ اقبال کا پہلا مجموعہ ہے جس کے سرورق پر انہوں نے کتاب کے نام اور
موضوع کی وضاحت کے لیے تو ضیحی الفاظ (اعلان جنگ دور حاضر کے خلاف)
درج کیے بلکہ ایک قطعے سے اس کی مزید تشریح بھی کی “(30)
علاج کے لیے بھو پال گئے تو شیش محل یا ریاض منزل میں لکھی جانے والی نظمیں بھی اس مجموعہ کلام میں شامل ہیں۔ ”ضرب کلیم“ کا مطالعہ اس بات کا منہ بولتا ثبوت ہے کہ شاعر مشرق پر شاعری کی دیوی مہربان ہے۔ حکیم الامت مرض الموت میں مبتلا ہو چکے ہیں مگر فکر وفن کا نزول جاری ہے۔
This paper presents the usage of Information Communication Technology (ICT) tools in Islamabad High Court (IHC) and determine the applications of ICT tools in the court. ICT plays vital role in the court processes. It has been adopted all over the world to enhance the performance of judiciary. The analyses are based on the primary collected data through survey questionnaire from judges, lawyers, clients, IT operators and administrative staff. The findings of the study revealed that ICT tools have been uses, particularly, basic IT tools such as computers etc. Are most commonly uses in the courts, however, it needs to use advance tools. Most of the respondents agreed that overall ICT tools have been adopted in the court. It is suggested for the IHC court to increase the judge’s ratio in the courts and bring judicial reforms in the system. The new findings and recommendations would be helpful for IHC.
Ablatives are materials used to protect the inner hardware of aerospace structures from the inimical temperature and shear environments. Fifty six diverse compositions have been used with numerous incorporations (MWCNTs, nanokaolinite, nanomontmorillonite, fine natural cork, phenolic resin, carbon fiber, Kevlar fiber, glass fiber, Spectra fiber, and ceramic fiber) and elastomeric matrices ( ethylene propylene monomer, styrene butadiene, silicon, and nitrile butadiene rubber) to fabricate polymer ablative composites for hyperthermal/hypersonic environment encountered during the space vehicle and ballistic missiles re-entry missions. The reinforcements have been impregnated into the elastomeric matrices using internal dispersion kneader and two-roller mixing mill. Three types of mold geometries have been used according to ASTM standards to fabricate the composites on the hot isostatic press to evaluate in-situ back-face temperature elevation, linear/radial ablation resistance, and mechanical properties. High temperature ( ≈ 3000 o C) oxy–acetylene torch coupled with the temperature data logging system was used to execute the ablation measurements of the ablative composites. Thermal stability and heat absorbing capability investigations have been carried out on the TG/DTA equipment. Mechanical properties have been executed using Universal Testing Machine (UTM) and rubber hardness tester. Scanning electron microscopy coupled with the energy dispersive spectroscopy was performed to demonstrate the reinforcement’s dispersion, interface quality, char morphology, char–reinforcement interaction, and compositional analysis of the composites. The ablation, thermal, and mechanical properties of the fabricated composites have been positively influenced with increasing the concentration of the nanoclays/synthetic fibers/nanotubes in the host rubber matrices. The least backface temperature evolution under 200s flame exposure, best linear/radial/mass ablation resistance, and the utmost improvement in tensile strength and elongation at break have been observed for 30 wt% nanokaolinite and 7 wt% chopped Kevlar fiber impregnated ablative composites. High thermal stability, heat quenching capability, low thermal conductivity, mechanical strength, and remarkable reinforcement–matrix adhesion are identified as the most viiprominent factors for enhanced ablation performance. The novelty of this research work is the fabrication of new ablative formulations with augmented ablation resistance (linear ablation rate of ~ 0.002mm/s) and back-face temperatures in the vicinity of 55 o C. This compares with the ablation rates of 0.01mm/s and back-face temperatures 130 o C for contemporary work using elastomeric composites under similar conditions. A host of ablators have been ranked in terms of linear and radial ablation rate, backface temperature, and mechanical strength following head-on impingement, or radial flow conditions of oxy- acetylene flame. The designer can choose the appropriate combination of ablators for the situation at hand using the ablation data provided in consolidated form towards the end of the thesis.