Flight Simulation Of HS-748 With And Without Rotodome Part-4 : Handling Qualities And Dynamic Responses

Padma, Madhuranatha and Sridhar, JK and Srinatha Sastry, CV and Krishnamurthy, K and Satyabhagavan, B (1990) Flight Simulation Of HS-748 With And Without Rotodome Part-4 : Handling Qualities And Dynamic Responses. Technical Report. NAL, Bangalore.

Full text available as:
[img] PDF
Download (69Kb)

    Abstract

    The Mathematical And Data Used In Off-Line Simulation Of The Rotodomed Aircraft Have Been Described In Detail In Part-1 . The Issue Related To The Rolls Royce Engine Simulation Studies Have Been Presented In Part-2 . The Formulation Of The Aerostatic 'Model And Its Verification Has Been Discussed In Part-3 . In This Report, The Results Of The Handling Qualities And Dynamic .Responses Of Both The Basic And The Aew Are Presented. The Results Are Discussed Within The Proposed Restricted C.G. Envelope And Speed Limits Of AEW.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Flight Simulation; Mathematical Modeling; Aircraft Unconventional Configuration Modeling; Dynamic Responses
    Subjects: ASTRONAUTICS > Astronautics (General)
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 10 Aug 2012 10:06
    Last Modified: 10 Aug 2012 10:06
    URI: http://nal-ir.nal.res.in/id/eprint/10776

    Actions (login required)

    View Item