Free Flight Experience Of The Lateral Stability Characteristics At Low Lift Of A 45 Swept Wing Rocket Propelled Model Equipped With A Nonlinear Yaw Rate Damper System At Mach Numbers From 0 76 To 1 73
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Free Flight Experience Of The Lateral Stability Characteristics At Low Lift Of A 45 Degree Swept Wing Rocket Propelled Model Equipped With A Nonlinear Yaw Rate Damper System At Mach Numbers From 0 76 To 1 73
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Author : Charles T. D'Aiutolo
language : en
Publisher:
Release Date : 1957
Free Flight Experience Of The Lateral Stability Characteristics At Low Lift Of A 45 Degree Swept Wing Rocket Propelled Model Equipped With A Nonlinear Yaw Rate Damper System At Mach Numbers From 0 76 To 1 73 written by Charles T. D'Aiutolo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Airplanes categories.
A low-lift lateral stability investigation was conducted with a rocket-propelled model of a 45 degree swept-wing-airplane configuration equipped with an auxiliary yaw-rate damper system in the Mach number range from 0.76 to 1.73. The lateral oscillations due to periodic yawing disturbances were analyzed to determine the lateral characteristics of the airframe-yaw-rate-damper combination. In addition, due to a dead spot in the operation of the yaw-rate damper system, it was possible to determine the lateral derivatives of the model when the Mach number was greater than 1.2 by the use of the time-vector method while the damper was essentially inoperative. The data were further interpreted in terms of full-scale-airplane flying qualities.
Free Flight Experience Of The Lateral Stability Characteristics At Low Lift Of A 45 Swept Wing Rocket Propelled Model Equipped With A Nonlinear Yaw Rate Damper System At Mach Numbers From 0 76 To 1 73
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Author : Charles T. D'Aiutolo
language : en
Publisher:
Release Date : 1957
Free Flight Experience Of The Lateral Stability Characteristics At Low Lift Of A 45 Swept Wing Rocket Propelled Model Equipped With A Nonlinear Yaw Rate Damper System At Mach Numbers From 0 76 To 1 73 written by Charles T. D'Aiutolo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Airplanes categories.
Lateral Stability Investigation At Mach Numbers From 0 8 To 1 7 Of Two Rocket Boosted Models Of An Airplane Configuration With A 45 Degree Swept Wing And A Low Horizontal Tail
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Author : John C. McFall
language : en
Publisher:
Release Date : 1957
Lateral Stability Investigation At Mach Numbers From 0 8 To 1 7 Of Two Rocket Boosted Models Of An Airplane Configuration With A 45 Degree Swept Wing And A Low Horizontal Tail written by John C. McFall and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Airplanes categories.
Rocket-boosted free-flight tests of two models of an airplane configuration having a 45 degree swept wing and a low horizontal-tail position have provided lateral stability derivatives and control effectiveness data for a Mach number range from 0.8 to 1.7. The experimental lateral stability derivatives presented are corrected to rigid conditions and compared with theoretically calculated rigid derivatives. The results are presented without detailed analysis.
Static Lateral Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane With Various Vertical Tails At Mach Numbers Of 1 41 1 61 And 2 01
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1956
Static Lateral Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane With Various Vertical Tails At Mach Numbers Of 1 41 1 61 And 2 01 written by M. Leroy Spearman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with categories.
Lateral Stability Characteristics At Low Lift Between Mach Numbers Of 0 85 And 1 15 Of A Rocket Propelled Model Of A Supersonic Airplane Configuration Having A Tapered Wing With Circular Arc Sections And 40 Degree Sweepback
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Author : Charles T. D'Aiutolo
language : en
Publisher:
Release Date : 1955
Lateral Stability Characteristics At Low Lift Between Mach Numbers Of 0 85 And 1 15 Of A Rocket Propelled Model Of A Supersonic Airplane Configuration Having A Tapered Wing With Circular Arc Sections And 40 Degree Sweepback written by Charles T. D'Aiutolo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with categories.
Static Lateral Stability And Control Characteristics Of A Model Of A 45 Swept Wing Fighter Airplane With Various Vertical Tails At Mach Numbers Of 1 41 1 61 And 2 01
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1956
Static Lateral Stability And Control Characteristics Of A Model Of A 45 Swept Wing Fighter Airplane With Various Vertical Tails At Mach Numbers Of 1 41 1 61 And 2 01 written by M. Leroy Spearman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Airplanes categories.
Rocket Model Investigation Of Lateral Stability Characteristics And Power Effects Of A Jet Engine Airplane Configuration With Tail Boom At Mach Numbers From 1 15 To 1 37
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Author : T. Bradley Curry (Jr)
language : en
Publisher:
Release Date : 1961
Rocket Model Investigation Of Lateral Stability Characteristics And Power Effects Of A Jet Engine Airplane Configuration With Tail Boom At Mach Numbers From 1 15 To 1 37 written by T. Bradley Curry (Jr) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.
Static Longitudinal Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane At Mach Numbers Of 1 41 1 61 And 2 01
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Author : Cornelius Driver
language : en
Publisher:
Release Date : 1956
Static Longitudinal Stability And Control Characteristics Of A Model Of A 45 Degree Swept Wing Fighter Airplane At Mach Numbers Of 1 41 1 61 And 2 01 written by Cornelius Driver and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamics, Supersonic categories.
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the static longitudinal stability and control characteristics of a model of a 45 degrees swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01.
The Effects Of Mass Distribution On The Low Speed Dynamic Lateral Stability And Control Characteristics Of A Model With 45 Degree Sweptback Wing
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Author :
language : en
Publisher:
Release Date : 1951
The Effects Of Mass Distribution On The Low Speed Dynamic Lateral Stability And Control Characteristics Of A Model With 45 Degree Sweptback Wing written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with categories.
Lateral Stability Characteristics Between Mach Numbers Of 0 80 And 1 57 And Simulation Of Coupled Motion At Mach Number Of 1 30 Of A Rocket Propelled Model Of An Airplane Configuration Having Thin Highly Tapered 45 Degree Sweptback Surfaces
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Author : Charles T. D'Aiutolo
language : en
Publisher:
Release Date : 1956
Lateral Stability Characteristics Between Mach Numbers Of 0 80 And 1 57 And Simulation Of Coupled Motion At Mach Number Of 1 30 Of A Rocket Propelled Model Of An Airplane Configuration Having Thin Highly Tapered 45 Degree Sweptback Surfaces written by Charles T. D'Aiutolo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Airplanes categories.
A rocket-propelled model of an airplane configuration having thin, highly tapered, 45 degree sweptback surfaces was tested in the Mach number range of 0.80 to 1.57 to obtain the lateral stability characteristics of the configuration.