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Works matching IS 00019240 AND DT 2006 AND VI 110 AND IP 1107

Results: 6

1

EPISTLE: High lift system design for low-noise applied to a supersonic aircraft.

Published in:

Aeronautical Journal, 2006, v. 110, n. 1107, p. 327, doi. 10.1017/S0001924000013191

By:

Herrmann, U.

Publication type:

Article

2

Aeroelastic analysis through linear and non-linear methods: a summary of flutter prediction in the PUMA DARP.

Published in:

Aeronautical Journal, 2006, v. 110, n. 1107, p. 333, doi. 10.1017/S0001924000013208

By:

Taylor, N. V.;
Allen, C. B.;
Gaitonde, A. L.;
Jones, D. P.;
Vio, G. A.;
Cooper, J. E.

Publication type:

Article

3

Active Control of a hybrid actuation system for aircraft vertical fin buffet load alleviation.

Published in:

Aeronautical Journal, 2006, v. 110, n. 1107, p. 315, doi. 10.1017/S000192400001318X

By:

Chen, Y.;
Wickramasinghe, V.;
Zimcik, D.

Publication type:

Article

4

CFD fire simulation of the Swissair Flight 111 in-flight fire — Part II: Fire spread analysis.

Published in:

Aeronautical Journal, 2006, v. 110, n. 1107, p. 303, doi. 10.1017/S0001924000013178

By:

Jia, F.;
Patel, M. K.;
Galea, E. A.;
Grandison, A.;
Ewer, J.

Publication type:

Article

5

Rigid body separation dynamics for space launch vehicles.

Published in:

Aeronautical Journal, 2006, v. 110, n. 1107, p. 289, doi. 10.1017/S0001924000013166

By:

Rao, B. N.;
Jeyakumar, O.;
Biswas, K. K.;
Swaminathan, S.;
Janardhana, E.

Publication type:

Article

6

Key aerodynamic technologies for aircraft engine nacelles.

Published in:

Aeronautical Journal, 2006, v. 110, n. 1107, p. 265, doi. 10.1017/S0001924000013154

By:

Raghunathan, S.;
Benard, E.;
Watterson, J. K.;
Cooper, A. K.;
Curran, R.;
Price, M.;
Yao, H.;
Devine, R.;
Crawford, B.;
Riordan, D.;
Linton, A.;
Richardson, J.;
Tweedie, J.

Publication type:

Article