A Rocket Model Investigation Of The Longitudinal Stability Lift And Drag Characteristics Of The Douglas X 3 Configuration With Horizontal Tail Of Aspect Ratio 4 33
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Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1957
Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.
A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1957
A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.
Research Abstracts And Reclassification Notice
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956
Research Abstracts And Reclassification Notice written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aeronautics categories.
Aeronautical Engineering Index
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Author :
language : en
Publisher:
Release Date : 1954
Aeronautical Engineering 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 1954 with Aeronautics categories.
Aviation Age Research And Development Technical Handbook
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Author :
language : en
Publisher:
Release Date : 1960
Aviation Age Research And Development Technical Handbook written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aeronautics categories.
Aerospace Engineering Index
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Author :
language : en
Publisher:
Release Date : 1960
Aerospace Engineering 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 1960 with Aeronautics categories.
A Rocket Model Investigation Of The Longitudinal Stability Lift And Drag Characteristics Of The Douglas X 3 Configuration With Horizontal Tail Of Aspect Ratio 4 33
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Author : Robert F. Peck
language : en
Publisher:
Release Date : 1953
A Rocket Model Investigation Of The Longitudinal Stability Lift And Drag Characteristics Of The Douglas X 3 Configuration With Horizontal Tail Of Aspect Ratio 4 33 written by Robert F. Peck and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with categories.
Rocket Model Investigation Of Longitudinal Stability And Drag Characteristics Of An Airplane Configuration Have A 60 Delta Wing And A High Unwept Horizontal Tail
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Author : Robert F. Peck
language : en
Publisher:
Release Date : 1953
Rocket Model Investigation Of Longitudinal Stability And Drag Characteristics Of An Airplane Configuration Have A 60 Delta Wing And A High Unwept Horizontal Tail written by Robert F. Peck and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Delta wing airplanes categories.
Rocket Model Investigation Of Longitudinal Stability And Drag Characteristics Of An Airplane Configuration Having A 60 Degree Delta Wing And A High Unswept Horizontal Tail
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Author : Robert F. Peck
language : en
Publisher:
Release Date : 1953
Rocket Model Investigation Of Longitudinal Stability And Drag Characteristics Of An Airplane Configuration Having A 60 Degree Delta Wing And A High Unswept Horizontal Tail written by Robert F. Peck and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 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.