Inlet Performance Characteristics Of A Generalized 1 4 Scale Tactical Aircraft Models At Transonic And Supersonic Mach Numbers
DOWNLOAD
Download Inlet Performance Characteristics Of A Generalized 1 4 Scale Tactical Aircraft Models At Transonic And Supersonic Mach Numbers PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Inlet Performance Characteristics Of A Generalized 1 4 Scale Tactical Aircraft Models At Transonic And Supersonic Mach Numbers book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Inlet Performance Characteristics Of A Generalized 1 4 Scale Tactical Aircraft Models At Transonic And Supersonic Mach Numbers
DOWNLOAD
Author : R. F. Lauer (Jr.)
language : en
Publisher:
Release Date : 1971
Inlet Performance Characteristics Of A Generalized 1 4 Scale Tactical Aircraft Models At Transonic And Supersonic Mach Numbers written by R. F. Lauer (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Aerodynamics, Supersonic categories.
Inlet Performance Characteristics Of A Generalized 1 5 2 Scale Aircraft Model At Transonic And Supersonic Mach Numbers
DOWNLOAD
Author : Jimmy Walker
language : en
Publisher:
Release Date : 1976
Inlet Performance Characteristics Of A Generalized 1 5 2 Scale Aircraft Model At Transonic And Supersonic Mach Numbers written by Jimmy Walker 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, Supersonic categories.
A wind tunnel investigation was conducted at free-stream Mach numbers from 0.55 to 2.0 on a 1/5.2-scale composite inlet model to evaluate configuration factors which affected inlet performance. In addition, flow-field surveys were made at the inlet throat and on the fuselage, forward of the inlet cowl lip. Inlet performance parameters in terms of total-pressure recovery, distortion, and turbulence at the simulated compressor face, as well as compressor face and throat station total-pressure contours and diffuser duct static-pressure distributions are presented for various Mach numbers and angles of attack and sideslip. The basic air induction system consisted of a normal-shock-type inlet with a long splitter plate assembly and was located beneath the wing glove in proximity to the fuselage. The total-pressure recovery for the basic inlet system was slightly better than normal shock recovery for cruise attitudes at supersonic Mach numbers. At Mach numbers approaching 2.0, the basic inlet system was operating close to the buzz limit at design engine airflow. Reductions in total-pressure distortion were achieved by increasing the fuselage-to-inlet standoff distance and by inlet duct boundary-layer blowing. (Author).
Aiaa 78 922 Aiaa 78 968
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1978
Aiaa 78 922 Aiaa 78 968 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Airplanes categories.
Technical Abstract Bulletin
DOWNLOAD
Author :
language : en
Publisher:
Release Date :
Technical Abstract Bulletin written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Science categories.
Air Frame Propulsion Interference Papers And Discussion Of The Fluid Dynamics Panel Symposium Held At Rome 3 6 September 1974
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1975
Air Frame Propulsion Interference Papers And Discussion Of The Fluid Dynamics Panel Symposium Held At Rome 3 6 September 1974 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 Aerodynamics categories.
Inlet Performance Characteristics Of A 1 5 Scale Northrop Yf 17 Model At Transonic And Supersonic Mach Numbers
DOWNLOAD
Author : M. E. Sanders
language : en
Publisher:
Release Date : 1974
Inlet Performance Characteristics Of A 1 5 Scale Northrop Yf 17 Model At Transonic And Supersonic Mach Numbers written by M. E. Sanders and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Cobra (Jet fighter plane) categories.
Scientific And Technical Aerospace Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1987
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 1987 with Aeronautics categories.
Results Of A 0 1 Scale B 1 Inlet Model Test At Transonic And Supersonic Mach Numbers
DOWNLOAD
Author : F. J. Graham
language : en
Publisher:
Release Date : 1971
Results Of A 0 1 Scale B 1 Inlet Model Test At Transonic And Supersonic Mach Numbers written by F. J. Graham and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Airplanes categories.
Results are presented of a wind tunnel investigation of a 0.1-scale model of the left-hand dual inlet air induction system of the B-1 aircraft. The test was conducted from Mach number 0.55 to 2.2 over an angle-of-attack range from -4 to 13 deg and yaw angles of -8 to 5 deg. Inlet performance in terms of compressor-face total-pressure recovery, total-pressure distortion, and turbulence index is presented as a function of inlet mass-flow ratios for various inlet geometries and model attitudes. The total-pressure recovery of the mixed-compression inlet was very good, but the total-pressure distortion at critical massflow ratios was higher than normally desired for satisfactory turbine engine operation. Best performance was realized with ramp and throat height schedules determined from previous testing. Effects of angle of attack and yaw were seen as general sidewash effects. The addition of canard-type fins had negligible effect on inlet performance. (Author).
Nasa Scientific And Technical Reports
DOWNLOAD
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1968
Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division 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.
A Selected Listing Of Nasa Scientific And Technical Reports
DOWNLOAD
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1969
A Selected Listing Of Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Aeronautics categories.