Comparison Of Low Lift Drag At Mach Numbers From 0 74 To 1 37 Of Rocket Boosted Models Having Externally Braced Wings And Cantilever Wings
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Comparison Of Low Lift Drag At Mach Numbers From 0 74 To 1 37 Of Rocket Boosted Models Having Externally Braced Wings And Cantilever Wings
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Author : Waldo L. Dickens
language : en
Publisher:
Release Date : 1957
Comparison Of Low Lift Drag At Mach Numbers From 0 74 To 1 37 Of Rocket Boosted Models Having Externally Braced Wings And Cantilever Wings written by Waldo L. Dickens and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerofoils categories.
An investigation has been conducted to determine whether the low-lift drag of a rocket-model airplane-like configuration could be reduced at transonic and low supersonic Mach numbers by reducing the wing thickness while external braces were used to provide the necessary bending strength. The investigation consisted of flight training two rocket models having aspect ratio 3.04, unswept braced tapered wings mounted on fuselages with the same fineness ratios and cross-sectional area distributions. Data collected from the flight test of a model having a thicker cantilever wing of the same plan form were compared with data collected in this investigation.
Free Flight Measurements Of The Zero Lift Drag Of Several Wings At Mach Numbers From 1 4 To 3 8
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Author : H. Herbert Jackson
language : en
Publisher:
Release Date : 1960
Free Flight Measurements Of The Zero Lift Drag Of Several Wings At Mach Numbers From 1 4 To 3 8 written by H. Herbert Jackson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Mach number categories.
Effects Of Inlet Modification And Rocket Rack Extension On The Longitudinal Trim And Low Lift Drag Of The Douglas F5d 1 Airplane As Obtained With A 0
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Author : Earl C. Hastings
language : en
Publisher: BiblioGov
Release Date : 2013-07
Effects Of Inlet Modification And Rocket Rack Extension On The Longitudinal Trim And Low Lift Drag Of The Douglas F5d 1 Airplane As Obtained With A 0 written by Earl C. Hastings and has been published by BiblioGov this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-07 with categories.
A flight investigation was conducted to determine the effects of an inlet modification and rocket-rack extension on the longitudinal trim and low-lift drag of the Douglas F5D-1 airplane. The investigation was conducted with a 0.125-scale rocket-boosted model which was flight tested at the Langley Pilotless Aircraft Research Station at Wallops Island, Va. Results indicate that the combined effects of the modified inlet and fully extended rocket racks on the trim lift coefficient and trim angle of attack were small between Mach numbers of 0.94 and 1.57. Between Mach numbers of 1.10 and 1.57 there was an average increase in drag coefficient of about o,005 for the model with modified inlet and extended rocket racks. The change in drag coefficient due to the inlet modification alone is small between Mach numbers of 1.59 and 1.64
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.
Drag Measurements Of A Reentry Body With Rocket Boosted Models In Free Flight At Mach Numbers From 2 8 To 0 6
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Author :
language : en
Publisher:
Release Date : 1959
Drag Measurements Of A Reentry Body With Rocket Boosted Models In Free Flight At Mach Numbers From 2 8 To 0 6 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 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.
Free Flight Drag Measurements Of Rocket Boosted Models Of Two Reentry Body Configurations At Mach Numbers From 4 3 To 0 6
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Author :
language : en
Publisher:
Release Date : 1959
Free Flight Drag Measurements Of Rocket Boosted Models Of Two Reentry Body Configurations At Mach Numbers From 4 3 To 0 6 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
Zero Lift Drag Measurements On Swept Wings At Transonic And Supersonic Speeds Using The Ground Launched Rocket Boosted Model Technique
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Author : T. Lawrence
language : en
Publisher:
Release Date : 1952
Zero Lift Drag Measurements On Swept Wings At Transonic And Supersonic Speeds Using The Ground Launched Rocket Boosted Model Technique written by T. Lawrence 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.
Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 70 To 1 37 Of Rocket Propelled Models Having A Modified Triangular Wing
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Author : Rowe Jr Chapman
language : en
Publisher:
Release Date : 1952
Longitudinal Stability And Drag Characteristics At Mach Numbers From 0 70 To 1 37 Of Rocket Propelled Models Having A Modified Triangular Wing written by Rowe Jr Chapman 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.