PARAMETRIC ANALYSIS AND PRELIMINARY DESIGN OF A SHAFT-DRIVEN ROTOR SYSTEM FOR A HEAVY LIFT HELICOPTER

Mapping Intimacies ◽

10.21236/ad0651416 ◽

1967 ◽

Cited By ~ 1

Author(s):

Walter J. Dutton

Keyword(s):

Parametric Analysis ◽

Rotor System ◽

Preliminary Design ◽

Heavy Lift

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PRELIMINARY DESIGN OF A ROTOR SYSTEM FOR A HOT CYCLE HEAVY-LIFT HELICOPTER

10.21236/ad0651217 ◽

1967 ◽

Author(s):

John R. Simpson

Keyword(s):

Rotor System ◽

Preliminary Design ◽

Heavy Lift

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HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 13. PRELIMINARY MODEL SPECIFICATION FOR CONTINENTAL MODEL 357-1 ENGINE

10.21236/ad0625823 ◽

1965 ◽

Author(s):

HILLER AIRCRAFT CORP PALO ALTO CA

Keyword(s):

Rotor System ◽

Model Specification ◽

Preliminary Model ◽

Heavy Lift ◽

System Volume

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HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 2. PARAMETRIC DESIGN STUDY

10.21236/ad0625819 ◽

1965 ◽

Author(s):

HILLER AIRCRAFT CORP PALO ALTO CA

Keyword(s):

Parametric Design ◽

Rotor System ◽

Design Study ◽

Heavy Lift ◽

System Volume

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HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 5. STRUCTURAL ANALYSIS

10.21236/ad0625820 ◽

1965 ◽

Author(s):

HILLER AIRCRAFT CORP PALO ALTO CA

Keyword(s):

Structural Analysis ◽

Rotor System ◽

Heavy Lift ◽

System Volume

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HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 10. STABILITY AND CONTROL

10.21236/ad0625822 ◽

1965 ◽

Author(s):

HILLER AIRCRAFT CORP PALO ALTO CA

Keyword(s):

Rotor System ◽

Stability And Control ◽

Heavy Lift ◽

And Control ◽

System Volume

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HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 9. PERFORMANCE ANALYSIS

10.21236/ad0625821 ◽

1965 ◽

Author(s):

HILLER AIRCRAFT CORP PALO ALTO CA

Keyword(s):

Performance Analysis ◽

Rotor System ◽

Heavy Lift ◽

System Volume

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HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 1

10.21236/ad0625818 ◽

1965 ◽

Author(s):

HILLER AIRCRAFT CORP PALO ALTO CA

Keyword(s):

Rotor System ◽

Heavy Lift ◽

System Volume

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PRELIMINARY DESIGN STUDY OF TIP-MOUNTED POWER PLANTS FOR THE MX-1660 HELICOPTER ROTOR SYSTEM

10.21236/ad0008257 ◽

1952 ◽

Author(s):

W. W. AVANT ◽

W. R. CUNNINGHAM

Keyword(s):

Power Plants ◽

Rotor System ◽

Helicopter Rotor ◽

Preliminary Design ◽

Design Study

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Preliminary Design of a Tip-Jet-Driven Heavy Lift Helicopter Incorporating Circulation Control

10.21236/ada099192 ◽

1981 ◽

Author(s):

R. E. Head

Keyword(s):

Preliminary Design ◽

Circulation Control ◽

Heavy Lift

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The Minnesota inverted-tee system: Parametric studies for preliminary design

PCI Journal ◽

10.15554/pcij.03012012.162.179 ◽

2012 ◽

Vol 57 (2) ◽

pp. 162-179

Author(s):

Roberto Piccinin ◽

Arturo E. Schultz

Keyword(s):

Preliminary Design ◽

Parametric Studies

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