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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Index To Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07
Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1987
Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Science categories.
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.
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.
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.
Flight Determined Static Lateral Stability And Control Characteristics Of A Swept Wing Fighter Airplane To A Mach Number Of 1 39
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Author : Gene J. Matranga
language : en
Publisher:
Release Date : 1957
Flight Determined Static Lateral Stability And Control Characteristics Of A Swept Wing Fighter Airplane To A Mach Number Of 1 39 written by Gene J. Matranga 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.
The static lateral stability characteristics of a swept-wing fighter-type airplane incorporating three vertical-tail configurations and two wing configurations were investigated at an altitude of 40,000 feet over a Mach number range from 0.72 to 1.39. The data obtained were determined during constant-heading sideslips and wings-level turns, aileron rolls, and abrupt rudder pulses.
Investigation Of The Dynamic Lateral Stability And Control Characteristics Of A Model Of A Fighter Airplane Without A Horizontal Tail And Equipped With Either Single Or Twin Vertical Tails
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Author : John W. Draper
language : en
Publisher:
Release Date : 1949
Investigation Of The Dynamic Lateral Stability And Control Characteristics Of A Model Of A Fighter Airplane Without A Horizontal Tail And Equipped With Either Single Or Twin Vertical Tails written by John W. Draper and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Airplanes categories.
Time Vector Determined Lateral Derivatives Of A Swept Wing Fighter Type Airplane With Three Different Vertical Tails At Mach Numbers Between 0 70 And 1 48
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Author : Chester H. Wolowicz
language : en
Publisher:
Release Date : 1956
Time Vector Determined Lateral Derivatives Of A Swept Wing Fighter Type Airplane With Three Different Vertical Tails At Mach Numbers Between 0 70 And 1 48 written by Chester H. Wolowicz 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.
As part of the flight research program conducted on a swept-wing fighter-type airplane, rudder-pulse maneuvers were performed at altitudes from 30,000 to 43,000 feet over a Mach number range of 0.71 to 1.48 to determine the lateral stability characteristics relative to the stability axes, in general, and the lateral derivative characteristics, in particular. The time-vector method of analysis was used. Four configurations were employed in the investigation. Three configurations involved three different vertical tails with varying aspect ratio or area, or both. The fourth configuration employed a large tail, which had been used in the third configuration, and an extension of the wing tips.
Static Longitudinal And Lateral Stability And Control Characteristics Of A Model Of A 35 Degree Swept Wing Airplane At A Mach Number Of 1 41
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Author : Edward B. Palazzo
language : en
Publisher:
Release Date : 1955
Static Longitudinal And Lateral Stability And Control Characteristics Of A Model Of A 35 Degree Swept Wing Airplane At A Mach Number Of 1 41 written by Edward B. Palazzo 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 Stability Characteristics At Mach Numbers From 1 90 To 4 63 Of A 76 Swept Arrow Wing Model With Variations In Horizontal Tail Height Wing Height And Dihedral
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Author : Dennis E. Fuller
language : en
Publisher:
Release Date : 1967
Static Stability Characteristics At Mach Numbers From 1 90 To 4 63 Of A 76 Swept Arrow Wing Model With Variations In Horizontal Tail Height Wing Height And Dihedral written by Dennis E. Fuller and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Airplanes categories.