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       Code No: RA212102
                                                                               RA
                  II B.Tech Supplimentary Examinations, Aug/Sep 2008
                FUNDAMENTALS OF AERONAUTICAL ENGINEERING
                                    (Aeronautical Engineering)
       Time: 3 hours                                                                   Max Marks: 80
                                   Answer any FIVE Questions
                                 All Questions carry equal marks



         1. (a) Explain the various engine-starting systems.                                           [10]
             (b) Discuss the contribution of Otto Lilienthal in the eld of aeronautics. Who
                  made the further contributions in the work eld of Otto Lilienthal ? Explain.
                                                                                                       [6]

         2. De ne an aircraft. How do you classify the various ight vehicles ? [16]

         3. Describe a rate of climb indicating instrument. How is it similar to or di erent
            from an Air speed indicator? Make use of sketches. -                                   [16]

         4. What is understood by the term “STABILITY OF ATMOSPHERE”? Work out
            the conditions under which atmosphere is stable.                                       [16]

         5. Discuss the di erent types of ribs and spars used in all metal aircraft wing. Also
            draw a neat sketch for each type.                                                      [16]

         6. What are the general types of construction of wings and fuselage, give practical
            examples of each type with neat sketches.                                              [16]

         7. What are the various components of turboprop engine? Describe them brie y.
            Discuss the di erent types of turboprop engines.                                       [16]

         8. What are the di erent types of rockets? Discuss their relative merits and applica-
            tions.
                                                                                                   [16]




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2102 Fundamentals Of Aeronautical Engineering Set1

  • 1. www.studentyogi.com www.studentyogi.com Code No: RA212102 RA II B.Tech Supplimentary Examinations, Aug/Sep 2008 FUNDAMENTALS OF AERONAUTICAL ENGINEERING (Aeronautical Engineering) Time: 3 hours Max Marks: 80 Answer any FIVE Questions All Questions carry equal marks 1. (a) Explain the various engine-starting systems. [10] (b) Discuss the contribution of Otto Lilienthal in the eld of aeronautics. Who made the further contributions in the work eld of Otto Lilienthal ? Explain. [6] 2. De ne an aircraft. How do you classify the various ight vehicles ? [16] 3. Describe a rate of climb indicating instrument. How is it similar to or di erent from an Air speed indicator? Make use of sketches. - [16] 4. What is understood by the term “STABILITY OF ATMOSPHERE”? Work out the conditions under which atmosphere is stable. [16] 5. Discuss the di erent types of ribs and spars used in all metal aircraft wing. Also draw a neat sketch for each type. [16] 6. What are the general types of construction of wings and fuselage, give practical examples of each type with neat sketches. [16] 7. What are the various components of turboprop engine? Describe them brie y. Discuss the di erent types of turboprop engines. [16] 8. What are the di erent types of rockets? Discuss their relative merits and applica- tions. [16] 1 of 1 www.studentyogi.com www.studentyogi.com