ACNP - Italian Periodicals Catalogue

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Results: 1-15 |

Results: 15

STATIC CONDENSATION IN MODAL-BASED STRUCTURAL OPTIMIZATION

Authors: MOULIN B KARPEL M

Citation: B. Moulin et M. Karpel, STATIC CONDENSATION IN MODAL-BASED STRUCTURAL OPTIMIZATION, Structural optimization, 15(3-4), 1998, pp. 275-283

INTEGRATED SOLUTION FOR COMPUTATIONAL STATIC AEROELASTICITY OF ROCKETS

Authors: KARPEL M YANIV S LIVSHITS DS

Citation: M. Karpel et al., INTEGRATED SOLUTION FOR COMPUTATIONAL STATIC AEROELASTICITY OF ROCKETS, Journal of spacecraft and rockets, 35(5), 1998, pp. 612-618

MODAL-BASED ENHANCEMENT OF INTEGRATED DESIGN OPTIMIZATION SCHEMES

Authors: KARPEL M

Citation: M. Karpel, MODAL-BASED ENHANCEMENT OF INTEGRATED DESIGN OPTIMIZATION SCHEMES, Journal of aircraft, 35(3), 1998, pp. 437-444

EXPERIMENTAL MODAL-ANALYSIS OF LARGE STRUCTURES BY SUBSTRUCTURING

Authors: KARPEL M RICCI S

Citation: M. Karpel et S. Ricci, EXPERIMENTAL MODAL-ANALYSIS OF LARGE STRUCTURES BY SUBSTRUCTURING, Mechanical systems and signal processing, 11(2), 1997, pp. 245-256

MODAL-BASED STRUCTURAL OPTIMIZATION WITH STATIC AEROELASTIC AND STRESS CONSTRAINTS

Authors: KARPEL M MOULIN B LOVE MH

Citation: M. Karpel et al., MODAL-BASED STRUCTURAL OPTIMIZATION WITH STATIC AEROELASTIC AND STRESS CONSTRAINTS, Journal of aircraft, 34(3), 1997, pp. 433-440

FLUTTER SENSITIVITY ANALYSIS USING RESIDUALIZATION FOR ACTIVELY CONTROLLED FLIGHT VEHICLES

Authors: HERSZBERG I KARPEL M

Citation: I. Herszberg et M. Karpel, FLUTTER SENSITIVITY ANALYSIS USING RESIDUALIZATION FOR ACTIVELY CONTROLLED FLIGHT VEHICLES, Structural optimization, 12(4), 1996, pp. 229-236

NONLINEAR FLUTTER ANALYSIS OF MISSILES WITH PNEUMATIC FIN ACTUATORS

Authors: YEHEZKELY E KARPEL M

Citation: E. Yehezkely et M. Karpel, NONLINEAR FLUTTER ANALYSIS OF MISSILES WITH PNEUMATIC FIN ACTUATORS, Journal of guidance, control, and dynamics, 19(3), 1996, pp. 664-670

GROUND MODAL TESTS OF SPACE-STRUCTURE COMPONENTS USING BOUNDARY MASSES

Authors: KARPEL M RAVEH D RICCI S

Citation: M. Karpel et al., GROUND MODAL TESTS OF SPACE-STRUCTURE COMPONENTS USING BOUNDARY MASSES, Journal of spacecraft and rockets, 33(2), 1996, pp. 272-277

MINIMUM-STATE UNSTEADY AERODYNAMIC APPROXIMATIONS WITH FLEXIBLE CONSTRAINTS

Authors: KARPEL M STRUL E

Citation: M. Karpel et E. Strul, MINIMUM-STATE UNSTEADY AERODYNAMIC APPROXIMATIONS WITH FLEXIBLE CONSTRAINTS, Journal of aircraft, 33(6), 1996, pp. 1190-1196

FICTITIOUS MASS ELEMENT IN STRUCTURAL DYNAMICS

Authors: KARPEL M RAVEH D

Citation: M. Karpel et D. Raveh, FICTITIOUS MASS ELEMENT IN STRUCTURAL DYNAMICS, AIAA journal, 34(3), 1996, pp. 607-613

STRUCTURAL DYNAMIC LOADS IN RESPONSE TO IMPULSIVE EXCITATION

Authors: KARPEL M PRESENTE E

Citation: M. Karpel et E. Presente, STRUCTURAL DYNAMIC LOADS IN RESPONSE TO IMPULSIVE EXCITATION, Journal of aircraft, 32(4), 1995, pp. 853-861

STRESS CONSIDERATIONS IN REDUCED-SIZE AEROELASTIC OPTIMIZATION

Authors: KARPEL M BRAININ L

Citation: M. Karpel et L. Brainin, STRESS CONSIDERATIONS IN REDUCED-SIZE AEROELASTIC OPTIMIZATION, AIAA journal, 33(4), 1995, pp. 716-722

CONTINUOUS GUST RESPONSE AND SENSITIVITY DERIVATIVES USING STATE-SPACE MODELS

Authors: ZOLE A KARPEL M

Citation: A. Zole et M. Karpel, CONTINUOUS GUST RESPONSE AND SENSITIVITY DERIVATIVES USING STATE-SPACE MODELS, Journal of aircraft, 31(5), 1994, pp. 1212-1214

MODAL COORDINATES FOR AEROELASTIC ANALYSIS WITH LARGE LOCAL STRUCTURAL VARIATIONS

Authors: KARPEL M WIESEMAN CD

Citation: M. Karpel et Cd. Wieseman, MODAL COORDINATES FOR AEROELASTIC ANALYSIS WITH LARGE LOCAL STRUCTURAL VARIATIONS, Journal of aircraft, 31(2), 1994, pp. 396-403

TIME SIMULATION OF FLUTTER WITH LARGE STIFFNESS CHANGES

Authors: KARPEL M WIESEMAN CD

Citation: M. Karpel et Cd. Wieseman, TIME SIMULATION OF FLUTTER WITH LARGE STIFFNESS CHANGES, Journal of aircraft, 31(2), 1994, pp. 404-410

Risultati: 1-15 |