Pressure Distribution Of A 0 0667 Scale Model Of The X 15 Airplane For An Angle Of Attack Range Of 0 To 28 At Mach Number Of 2 30 2 88 And 4 65
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Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1968
Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Aeronautics categories.
Pressure Distribution Of A 0 0667 Scale Model Of The X 15 Airplane For An Angle Of Attack Range Of 0 Deg To 28 Deg At Mach Numbers Of 2 30 2 88 And 4 65
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Author :
language : en
Publisher:
Release Date : 1960
Pressure Distribution Of A 0 0667 Scale Model Of The X 15 Airplane For An Angle Of Attack Range Of 0 Deg To 28 Deg At Mach Numbers Of 2 30 2 88 And 4 65 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 categories.
Pressure Distribution Of A 0 0667 Scale Model Of The X 15 Airplane For An Angle Of Attack Range Of 0 To 28 At Mach Number Of 2 30 2 88 And 4 65
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Author : Leon B. Hodge
language : en
Publisher:
Release Date : 1960
Pressure Distribution Of A 0 0667 Scale Model Of The X 15 Airplane For An Angle Of Attack Range Of 0 To 28 At Mach Number Of 2 30 2 88 And 4 65 written by Leon B. Hodge and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.
Pressure Distribution Of A 0 0667 Scale Model Of The X 15 Airplane For An Angle Of Attack Range Of 0 To 28 At Mach Numbers Of 2 30 288 And 4 65
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Author : B. Leon Hodge
language : en
Publisher:
Release Date : 1960
Pressure Distribution Of A 0 0667 Scale Model Of The X 15 Airplane For An Angle Of Attack Range Of 0 To 28 At Mach Numbers Of 2 30 288 And 4 65 written by B. Leon Hodge and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aerodynamic load categories.
Aerodynamic Characteristics Of A 0 0667 Scale Model Of The X 15a 2 Research Airplane At Transonic Speeds
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Author : James C. Patterson
language : en
Publisher:
Release Date : 1966
Aerodynamic Characteristics Of A 0 0667 Scale Model Of The X 15a 2 Research Airplane At Transonic Speeds written by James C. Patterson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.
Experimental Surface Pressure Data Obtained On 65 Delta Wing Across Reynolds Number And Mach Number Ranges
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Author : Julio Chu
language : en
Publisher:
Release Date : 1996
Experimental Surface Pressure Data Obtained On 65 Delta Wing Across Reynolds Number And Mach Number Ranges written by Julio Chu and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Angle of attack categories.
Pressure Distributions On A Flat Plate Delta Wing Swept 65 Deg At A Mach Number Of 5 97 At Angles Of Attack From 65 Deg To 115 Deg And Angles Of Roll From 0 Deg To 25 Deg At A 90 Deg Angle Of Attack
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Author :
language : en
Publisher:
Release Date : 1962
Pressure Distributions On A Flat Plate Delta Wing Swept 65 Deg At A Mach Number Of 5 97 At Angles Of Attack From 65 Deg To 115 Deg And Angles Of Roll From 0 Deg To 25 Deg At A 90 Deg Angle Of Attack written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with categories.
Preliminary Base Pressures Obtained From The X 15 Airplane At Mach Numbers From 1 1 To 3 2
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Author : Edwin J. Saltzman
language : en
Publisher:
Release Date : 1961
Preliminary Base Pressures Obtained From The X 15 Airplane At Mach Numbers From 1 1 To 3 2 written by Edwin J. Saltzman 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.
Base Pressure Coefficients Obtained From The X 15 Airplane For Mach Numbers Up To 6
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Author : Edwin J. Saltzman
language : en
Publisher:
Release Date : 1964
Base Pressure Coefficients Obtained From The X 15 Airplane For Mach Numbers Up To 6 written by Edwin J. Saltzman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aerodynamics, Supersonic categories.
Measured And Calculated Flow Conditions On The Forward Fuselage Of The X 15 Airplane And Model At Mach Numbers From 3 0 To 8 0
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Author : Murray Palitz
language : en
Publisher:
Release Date : 1966
Measured And Calculated Flow Conditions On The Forward Fuselage Of The X 15 Airplane And Model At Mach Numbers From 3 0 To 8 0 written by Murray Palitz and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamics, Hypersonic categories.