Lift Drag And Longitudinal Stability At Mach Numbers From 1 4 To 2 3 Of A Rocket Powered Model Having A 52 5 Degree Sweptback Wing Of Aspect Ratio 3 And Inline Tail Surfaces

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Lift Drag And Longitudinal Stability At Mach Numbers From 1 4 To 2 3 Of A Rocket Powered Model Having A 52 5 Degree Sweptback Wing Of Aspect Ratio 3 And Inline Tail Surfaces

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Author : Warren Jr Gillespie
language : en
Publisher:
Release Date : 1955

Lift Drag And Longitudinal Stability At Mach Numbers From 1 4 To 2 3 Of A Rocket Powered Model Having A 52 5 Degree Sweptback Wing Of Aspect Ratio 3 And Inline Tail Surfaces written by Warren Jr Gillespie 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.

Lift Drag And Longitudinal Stability At Mach Numbers From 0 8 To 2 1 Of A Rocket Powered Model Having A Tapered Unswept Wing Of Aspect Ratio 3 And Inline Tail Surfaces

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Author : Warren Jr Gillespie
language : en
Publisher:
Release Date : 1955

Lift Drag And Longitudinal Stability At Mach Numbers From 0 8 To 2 1 Of A Rocket Powered Model Having A Tapered Unswept Wing Of Aspect Ratio 3 And Inline Tail Surfaces written by Warren Jr Gillespie 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.

Stability Of Two Rocket Propelled Models Having Aspect Ratio 5 Unswept Tails On A Long Body For The Mach Number Range Of 1 7 To 2 4

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Author : Reginald R. Lundstrom
language : en
Publisher:
Release Date : 1957

Stability Of Two Rocket Propelled Models Having Aspect Ratio 5 Unswept Tails On A Long Body For The Mach Number Range Of 1 7 To 2 4 written by Reginald R. Lundstrom and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamics, Supersonic categories.

Two rocket models having cruciform, aspect-ratio-5, unwswept tails and a fineness-ratio-20 fuselage were flight tested over a Mach number range of approximately 1.7 to 2.4. One of the models had cruciform, aspect-ratio-3.4 forward surfaces in line with the tails. The models were given step disturbances by pulse rockets at intervals throughout the Mach number range and stability derivatives were obtained from the measured responses. The roll rates of the models varied from 10 radians per second to 5 radians per second.

Longitudinal Stability And Trim Of Two Rocket Propelled Airplane Models Having 45 Sweptback Wings And Tails With The Horizontal Tail Mounted In Two Positions

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Author : James H. Parks
language : en
Publisher:
Release Date : 1953

Longitudinal Stability And Trim Of Two Rocket Propelled Airplane Models Having 45 Sweptback Wings And Tails With The Horizontal Tail Mounted In Two Positions written by James H. Parks and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.

Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 75 To 1 5 Of An Airplane Configuration Having A 60 Degrees Swept Wing Of Aspect Ratio 2 24 As Obtained From Rocket Propelled Model

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Author : A. James Vitale
language : en
Publisher:
Release Date : 1952

Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 75 To 1 5 Of An Airplane Configuration Having A 60 Degrees Swept Wing Of Aspect Ratio 2 24 As Obtained From Rocket Propelled Model written by A. James Vitale and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.

Rocket Powered Model Investigation Of Lift Drag And Stability Of A Body Tail Configuration At Mach Numbers From 0 8 To 2 3 And Angles Of Attack Between Plus Or Minus 6 5 Degrees

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Author : Warren Jr Gillespie
language : en
Publisher:
Release Date : 1954

Rocket Powered Model Investigation Of Lift Drag And Stability Of A Body Tail Configuration At Mach Numbers From 0 8 To 2 3 And Angles Of Attack Between Plus Or Minus 6 5 Degrees written by Warren Jr Gillespie and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with categories.

Large Scale Flight Measurements Of Zero Lift Drag And Low Lift Drag Of 10 Wing Body Configurations At Mach Numbers From 0 8 To 1 6

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Author : John D. Morrow
language : en
Publisher:
Release Date : 1953

Large Scale Flight Measurements Of Zero Lift Drag And Low Lift Drag Of 10 Wing Body Configurations At Mach Numbers From 0 8 To 1 6 written by John D. Morrow and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.

Longitudinal Stability Trim And Drag Characteristics Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Sweptback Wing And An Unswept Horizontal Tail

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Author : James H. Parks
language : en
Publisher:
Release Date : 1952

Longitudinal Stability Trim And Drag Characteristics Of A Rocket Propelled Model Of An Airplane Configuration Having A 45 Degree Sweptback Wing And An Unswept Horizontal Tail written by James H. Parks and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with categories.

Aerodynamic Characteristics At Mach Numbers From 0 50 To 2 96 Of A Supersonic Transport Model With A Variable Sweep High Panel Aspect Ratio Wing

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Author :
language : en
Publisher:
Release Date : 1964

Aerodynamic Characteristics At Mach Numbers From 0 50 To 2 96 Of A Supersonic Transport Model With A Variable Sweep High Panel Aspect Ratio 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 1964 with categories.

Lift Drag Static Stability And Buffet Boundaries Of A Model Of The Mcdonnell F3h 1n Airplane At Mach Numbers From 0 40 To 1 27 Ted No Naca De 351

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Author : Norman L. Crabill
language : en
Publisher: BiblioGov
Release Date : 2013-06

Lift Drag Static Stability And Buffet Boundaries Of A Model Of The Mcdonnell F3h 1n Airplane At Mach Numbers From 0 40 To 1 27 Ted No Naca De 351 written by Norman L. Crabill and has been published by BiblioGov this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-06 with categories.

The National Advisory Committee for Aeronautics has conducted a flight test of a model approximating the McDonnell F3H-lN airplane configuration to determine its pitch-up and buffet boundaries, as well as the usual longitudinal stability derivatives obtainable from the pulsed- tail technique. The test was conducted by the freely flying rocket- boosted model technique developed at the Langley Laboratory; results were obtained at Mach numbers from 0.40 to 1.27 at corresponding Reynolds numbers of 2.6 x 10(exp 6) and 9.0 x 10(exp 6). The phenomena of pitch-up, buffet, and maximum lift were encountered at Mach numbers between 0.42 and 0.85. The lift-curve slope and wing-root bending-moment slope increased with increasing angle of attack, whereas the static stability decreased with angle of attack at subsonic speeds and increased at transonic speeds. There was little change in trim at low lift at transonic speeds.