Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Various Noses At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0
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Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Various Noses At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0
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Author : Leland Howard Jorgensen
language : en
Publisher:
Release Date : 1974
Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Various Noses At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0 written by Leland Howard Jorgensen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Aerodynamics categories.
Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Side Strakes And Various Noses At Angle Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0
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Author : Leland H. Jorgensen
language : en
Publisher:
Release Date : 1975
Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Side Strakes And Various Noses At Angle Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0 written by Leland H. Jorgensen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.
Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Side Strakes And Various Noses At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0
DOWNLOAD
Author : Leland H. Jorgensen
language : en
Publisher:
Release Date : 1975
Experimental Aerodynamic Characteristics For A Cylindrical Body Of Revolution With Side Strakes And Various Noses At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0 written by Leland H. Jorgensen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamics categories.
Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1979
Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aeronautics categories.
Experimental Aerodynamic Characteristics For Slender Bodies With Thin Wings And Tail At Angles Of Attack From 0 To 58 And Mach From 0 6 To 2 0
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Author : Leland H. Jorgensen
language : en
Publisher:
Release Date : 1976
Experimental Aerodynamic Characteristics For Slender Bodies With Thin Wings And Tail At Angles Of Attack From 0 To 58 And Mach From 0 6 To 2 0 written by Leland H. Jorgensen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Aerodynamics categories.
Experimental Aerodynamic Characteristics For Slender Bodies With Thin Wings At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0
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Author : Leland H. Jorgensen
language : en
Publisher:
Release Date : 1976
Experimental Aerodynamic Characteristics For Slender Bodies With Thin Wings At Angles Of Attack From 0 To 58 And Mach Numbers From 0 6 To 2 0 written by Leland H. Jorgensen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Aerodynamics categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1979
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aeronautics categories.
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.
Side Forces On A Tangent Ogive Forebody With A Fineness Ratio Of 2 5 At High Angles Of Attack And Low Speed
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Author :
language : en
Publisher:
Release Date : 1976
Side Forces On A Tangent Ogive Forebody With A Fineness Ratio Of 2 5 At High Angles Of Attack And Low Speed written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with categories.
Wind Tunnel Investigation Of The Aerodynamic Characteristics Of Five Forebody Models At High Angles Of Attack At Mach Numbers From 0 25 To 2
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Author :
language : en
Publisher:
Release Date : 1975
Wind Tunnel Investigation Of The Aerodynamic Characteristics Of Five Forebody Models At High Angles Of Attack At Mach Numbers From 0 25 To 2 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.