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Book An Axisymmetric Analog Two layer Convective Heating Procedure with Application to the Evaluation of Space Shuttle Orbiter Wing Leading Edge and Windward Surface Heating

Download or read book An Axisymmetric Analog Two layer Convective Heating Procedure with Application to the Evaluation of Space Shuttle Orbiter Wing Leading Edge and Windward Surface Heating written by and published by . This book was released on 1994 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Axisymmetric Analog Two Layer Convective Heating Procedure with Application to the Evaluation of Space Shuttle Orbiter Wing Leading Edge and Windward Surface Heating

Download or read book An Axisymmetric Analog Two Layer Convective Heating Procedure with Application to the Evaluation of Space Shuttle Orbiter Wing Leading Edge and Windward Surface Heating written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical procedure for predicting the convective heating rate of hypersonic reentry vehicles is described. The procedure, which is based on the axisymmetric analog, consists of obtaining the three-dimensional inviscid flowfield solution; then the surface streamlines and metrics are calculated using the inviscid velocity components on the surface; finally, an axisymmetric boundary layer code or approximate convective heating equations are used to evaluate heating rates. This approach yields heating predictions to general three-dimensional body shapes. The procedure has been applied to the prediction of the wing leading edge heating to the Space Shuttle Orbiter. The numerical results are compared with the results of heat transfer testing (OH66) of an 0.025 scale model of the Space Shuttle Orbiter configuration in the Calspan Hypersonic Shock Tunnel (HST) at Mach 10 and angles of attack of 30 and 40 degrees. Comparisons with STS-5 flight data at Mach 9.15 and angle of attack of 37.4 degrees and STS-2 flight data at Mach 12.86 and angle of attack of 39.7 degrees are also given. Wang, K. C. Unspecified Center AERODYNAMIC HEATING; COMPUTATIONAL FLUID DYNAMICS; CONVECTIVE HEAT TRANSFER; HYPERSONIC HEAT TRANSFER; INVISCID FLOW; SPACE SHUTTLE ORBITERS; ANGLE OF ATTACK; BOUNDARY LAYERS; HYPERSONIC SPEED; LEADING EDGES; THREE DIMENSIONAL BODIES...

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book 32nd Thermophysics Conference

Download or read book 32nd Thermophysics Conference written by and published by . This book was released on 1997 with total page 734 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book 31st AIAA Thermophysics Conference

Download or read book 31st AIAA Thermophysics Conference written by and published by . This book was released on 1996 with total page 730 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book 34th Aerospace Sciences Meeting Exhibit

Download or read book 34th Aerospace Sciences Meeting Exhibit written by and published by . This book was released on 1996 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Announcements Index

Download or read book Government Reports Announcements Index written by and published by . This book was released on 1995 with total page 624 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft

Download or read book A Method for Calculating Transient Surface Temperatures and Surface Heating Rates for High speed Aircraft written by Robert D. Quinn and published by . This book was released on 2000 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a method that can calculate transient aerodynamic heating and transient surface temperatures at supersonic and hypersonic speeds. This method can rapidly calculate temperature and heating rate time-histories for complete flight trajectories. Semi-empirical theories are used to calculate laminar and turbulent heat transfer coefficients and a procedure for estimating boundary-layer transition is included. Results from this method are compared with flight data from the X-15 research vehicle, YF-12 airplane, and the Space Shuttle Orbiter. These comparisons show that the calculated values are in good agreement with the measured flight data.

Book Experimental Aerodynamic Heating to Simulated Space Shuttle Tiles in Laminar and Turbulent Boundary Layers with Variable Flow Angles at a Nominal Mach Number of 7

Download or read book Experimental Aerodynamic Heating to Simulated Space Shuttle Tiles in Laminar and Turbulent Boundary Layers with Variable Flow Angles at a Nominal Mach Number of 7 written by Don E. Avery and published by . This book was released on 1985 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Heating of a Space Shuttle Delta wing Orbiter

Download or read book Aerodynamic Heating of a Space Shuttle Delta wing Orbiter written by and published by . This book was released on 1971 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aeroheating Predictions for X 34 Using an Inviscid Boundary Layer Method

Download or read book Aeroheating Predictions for X 34 Using an Inviscid Boundary Layer Method written by Christropher J. Riley and published by . This book was released on 1998 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: