The Zero Lift Drag Of A 60 Degrees Delta Wing Body Combination Agard Model 2 Obtained From Free Flight Tests Between Mach Numbers Of 0 8 And 1 7
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Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1966
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 1966 with Aeronautics categories.
The Journal Of The Royal Aeronautical Society
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Author :
language : en
Publisher:
Release Date : 1961
The Journal Of The Royal Aeronautical Society written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aeronautics categories.
Journal Of The Royal Aeronautical Society
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Author :
language : en
Publisher:
Release Date : 1961
Journal Of The Royal Aeronautical Society written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Aeronautics categories.
The Zero Lift Drag Of A 60 Degree Delta Wing Body Combination Agard Model 2 Obtained From Free Flight Tests Between Mach Numbers Of 0 8 And 1 7
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Author : Robert O. Piland
language : en
Publisher:
Release Date : 1954
The Zero Lift Drag Of A 60 Degree Delta Wing Body Combination Agard Model 2 Obtained From Free Flight Tests Between Mach Numbers Of 0 8 And 1 7 written by Robert O. Piland and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.
The zero-lift drag of a 60 degree delta-wing-body combination (designated AGARD Model 2) has been determined by free-flight tests of two models between Mach numbers of 0.8 and 1.7. These Mach numbers correspond to Reynolds numbers, based on body length, of 4,000,000 and 12,000,000, respectively. An estimate of the drag of the configuration was made by summing the estimates of the drag of the various components. The agreement between measured and estimated drag is good.
The Zero Lift Drag Of A 60 Degrees Delta Wing Body Combination Agard Model 2 Obtained From Free Flight Tests Between Mach Numbers Of 0 8 And 1 7
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Author : Robert O. Piland
language : en
Publisher:
Release Date : 1954
The Zero Lift Drag Of A 60 Degrees Delta Wing Body Combination Agard Model 2 Obtained From Free Flight Tests Between Mach Numbers Of 0 8 And 1 7 written by Robert O. Piland 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.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1987
Government Reports Announcements 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 1987 with Science 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.
Investigation Of Lift Drag And Pitching Moment Of A 60 Deg Delta Wing Body Combination Agard Calibration Model B In The Langley 9 Inch Supersonic Tunnel
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Author :
language : en
Publisher:
Release Date : 1954
Investigation Of Lift Drag And Pitching Moment Of A 60 Deg Delta Wing Body Combination Agard Calibration Model B In The Langley 9 Inch Supersonic Tunnel 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 categories.
The lift, drag, and pitching-moment characteristics of the AGARD Calibration Model B as determined in the Langley 9-inch supersonic tunnel are presented at Mach numbers of 1.62, 1.94, and 2.41 and at a Reynolds number, based on body length, of approximately 3.0 x 10(exp 6). The zero-lift drag data compared favorably with available data and were in the proper sequence for the effects of Reynolds number.
The Effect Of Inlet Installation On The Zero Lift Drag Of A 60 Degree Delta Wing Body Configuration From Flight Tests At Mach Numbers From 0 8 To 1 86
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Author : Charles F. Merlet
language : en
Publisher:
Release Date : 1955
The Effect Of Inlet Installation On The Zero Lift Drag Of A 60 Degree Delta Wing Body Configuration From Flight Tests At Mach Numbers From 0 8 To 1 86 written by Charles F. Merlet 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.
The Effect Of Inlet Installation Of The Zero Lift Drag Of A 60 Delta Wing Body Configuration From Flight Tests At Mach Numbers From 0 8 To 1 86
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Author : Charles F. Merlet
language : en
Publisher:
Release Date : 1958
The Effect Of Inlet Installation Of The Zero Lift Drag Of A 60 Delta Wing Body Configuration From Flight Tests At Mach Numbers From 0 8 To 1 86 written by Charles F. Merlet and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Airplanes categories.