Turbulent Reentry

Download Turbulent Reentry PDF Online Free

Author :
Publisher : Lulu.com
ISBN 13 : 1329629701
Total Pages : 128 pages
Book Rating : 4.07/5 ( download)

DOWNLOAD NOW!


Book Synopsis Turbulent Reentry by : Kyle Fisher

Download or read book Turbulent Reentry written by Kyle Fisher and published by Lulu.com. This book was released on with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Hypersonic Flows for Reentry Problems

Download Hypersonic Flows for Reentry Problems PDF Online Free

Author :
Publisher : Springer Science & Business Media
ISBN 13 : 3642765270
Total Pages : 1231 pages
Book Rating : 4.78/5 ( download)

DOWNLOAD NOW!


Book Synopsis Hypersonic Flows for Reentry Problems by : Jean-Antoine Desideri

Download or read book Hypersonic Flows for Reentry Problems written by Jean-Antoine Desideri and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 1231 pages. Available in PDF, EPUB and Kindle. Book excerpt: This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as "MANDATORY" and some as "OPTIONAL" for the purposes of CFD validation. However, only the "MANDATORY" data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59.

Prediction of the Pressure Fluctuations Associated with Maneuvering Reentry Weapons

Download Prediction of the Pressure Fluctuations Associated with Maneuvering Reentry Weapons PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 184 pages
Book Rating : 4.7E/5 ( download)

DOWNLOAD NOW!


Book Synopsis Prediction of the Pressure Fluctuations Associated with Maneuvering Reentry Weapons by : Anthony L. Laganelli

Download or read book Prediction of the Pressure Fluctuations Associated with Maneuvering Reentry Weapons written by Anthony L. Laganelli and published by . This book was released on 1984 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental program was conducted at the AEDC von Karman facility, Tunnels A and B, in which acoustic pressure fluctuation data were acquired on a 7 degree half-cone-angle model featuring a control surface. The objective was to define the aeroacoustic environment applicable to re-entry vibration response analysis for both ballistic and maneuvering vehicles. Wind tunnel measurements were obtained at Mach 4 and 8 for several values of freestream Reynolds number and model angle of attack. Stationary zones of laminar, transitional, and turbulent flow over the model were achieved. Acoustic data were reduced to rms fluctuating pressure, and power and cross-power spectral densities. Results were normalized using local boundary layer parameters for comparison with previous high speed measurements. The present study re-examined the aeroacoustic environment prediction capability relative to compressible flow conditions. Moreover, boundary layer characteristic lengths and velocities were reviewed in order to develop normalization procedures required for development of appropriate aeroacoustic scaling laws. It was determined that fluctuating pressure characteristics described by incompressible theory as well as empirical correlations could be modified to a compressible state through a transformation function. In this manner, compressible data were transformed to the incompressible plane where direct use of more tractable prediction techniques are available for engineering design analyses.

Scientific and Technical Aerospace Reports

Download Scientific and Technical Aerospace Reports PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 290 pages
Book Rating : 4.58/5 ( download)

DOWNLOAD NOW!


Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 290 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Abstract Bulletin

Download Technical Abstract Bulletin PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 908 pages
Book Rating : 4.93/5 ( download)

DOWNLOAD NOW!


Book Synopsis Technical Abstract Bulletin by :

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 908 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Calculation of the Subsonic and Transonic Turbulent Boundary Layer on an Infinite Yawed Airfoil

Download Numerical Calculation of the Subsonic and Transonic Turbulent Boundary Layer on an Infinite Yawed Airfoil PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.28/5 ( download)

DOWNLOAD NOW!


Book Synopsis Numerical Calculation of the Subsonic and Transonic Turbulent Boundary Layer on an Infinite Yawed Airfoil by : John C. Adams (Jr.)

Download or read book Numerical Calculation of the Subsonic and Transonic Turbulent Boundary Layer on an Infinite Yawed Airfoil written by John C. Adams (Jr.) and published by . This book was released on 1973 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Reentry-F Flowfield Solutions at 80,000 Ft

Download Reentry-F Flowfield Solutions at 80,000 Ft PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.27/5 ( download)

DOWNLOAD NOW!


Book Synopsis Reentry-F Flowfield Solutions at 80,000 Ft by :

Download or read book Reentry-F Flowfield Solutions at 80,000 Ft written by and published by . This book was released on 1997 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Uniform Roughness Studies

Download Uniform Roughness Studies PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.32/5 ( download)

DOWNLOAD NOW!


Book Synopsis Uniform Roughness Studies by : David Edward Klett

Download or read book Uniform Roughness Studies written by David Edward Klett and published by . This book was released on 1992 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Juvenile Offending

Download Juvenile Offending PDF Online Free

Author :
Publisher : Taylor & Francis
ISBN 13 : 1000944379
Total Pages : 343 pages
Book Rating : 4.72/5 ( download)

DOWNLOAD NOW!


Book Synopsis Juvenile Offending by : Thom Brooks

Download or read book Juvenile Offending written by Thom Brooks and published by Taylor & Francis. This book was released on 2023-05-31 with total page 343 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tackling juvenile offending has become a key part of crime reduction strategies. The articles selected for this volume examine juvenile offending from various critical perspectives and represent the work of the most influential international figures in the field. The issues addressed include: the different needs and perspectives of youth offenders; whether offenders should be treated differently from others because of their age; recommendations of policy changes; identification of risk factors; issues surrounding the sentencing of juvenile offenders; and the relevance of restorative justice.

The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles

Download The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.31/5 ( download)

DOWNLOAD NOW!


Book Synopsis The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles by : E. C. Lemmon

Download or read book The Prediction of Aerodynamic Heating of Fins on Re-entry Vehicles written by E. C. Lemmon and published by . This book was released on 1971 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: