Moment stability Derivatives of N A G Missile Configuration-at Low Speed using Semi-free Dynamic Flying
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Moment stability Derivatives of N A G Missile Configuration-at Low Speed using Semi-free Dynamic Flying
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| Creator |
Balakrishna, S
Niranjana, T Rajan, SR |
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| Subject |
Aircraft Design, Testing & Performance
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| Description |
Dynamic flying of scaled model exploits the advantages of flight test methodology and wind tunnel flexibility to generate stability derivative data in evaluated using dynamic
flying A 1 : 1 .45 scaled model is flown in a low speed, tunnel and its pitching response to servoed tail drive doublet is analysed using Maximum Likelihood Estimation method . The results indicate a low angle of attack static instability for the tested configuration.
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| Publisher |
NAL
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| Type |
Proj.Doc/Technical Report
NonPeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/10582/1/PD_SE_8917.pdf
Balakrishna, S and Niranjana, T and Rajan, SR Moment stability Derivatives of N A G Missile Configuration-at Low Speed using Semi-free Dynamic Flying. Project Report. NAL, Bangalore. |
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| Relation |
http://nal-ir.nal.res.in/10582/
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