A Method For Predicting Pressures On Elliptic Cones At Supersonic Speeds
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Author | : George E. Kaattari |
Publisher | : |
Total Pages | : 36 |
Release | : 1970 |
Genre | : Aerodynamic load |
ISBN | : |
Download A Method for Predicting Pressures on Elliptic Cones at Supersonic Speeds Book in PDF, Epub and Kindle
Author | : George E. Kaattari |
Publisher | : |
Total Pages | : 23 |
Release | : 1970 |
Genre | : Aerodynamic load |
ISBN | : |
Download A Method for Predicting Pressures on Elliptic Cones at Supersonic Speeds Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 478 |
Release | : 1973 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Technical Note Book in PDF, Epub and Kindle
Author | : George E. Kaattari |
Publisher | : |
Total Pages | : 28 |
Release | : 1971 |
Genre | : Angle of attack (Aerodynamics) |
ISBN | : |
Download Prediction of Centerline Shock-layer Thickness and Pressure Distribution on Delta Wing-body Configurations Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 758 |
Release | : 1970 |
Genre | : Aerodynamics |
ISBN | : |
Download Analytic Methods in Aircraft Aerodynamics Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1460 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, Epub and Kindle
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author | : |
Publisher | : |
Total Pages | : 580 |
Release | : 1971 |
Genre | : Aeronautics |
ISBN | : |
Download Aeronautical Engineering Book in PDF, Epub and Kindle
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Author | : Martin C. Jischke |
Publisher | : |
Total Pages | : 414 |
Release | : 1981 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Aerodynamics of Supersonic Lifting Bodies Book in PDF, Epub and Kindle
This report describes a combined theoretical and experimental program of research in the aerodynamics of supersonic lifting bodies. Analytical perturbation techniques are used to study the supersonic flow past slightly elliptical cones, cones whose cross-sections deviate slightly but arbitrarily from that of a right circular cone, cones of small longitudinal curvature, and right circular cones undergoing small harmonic pitching and/or plunging motions. These studies all involve perturbations of the well-known solution for supersonic flow past a right circular cone. Closed-form analytical results are achieved through the use of an approximation that accurately predicts results over the entire range of the hypersonic similarity parameter. These results give hypersonic limiting solutions that agree well with other independent analyses and, at the same time, agree exactly with linearized theory in the linear theory limit. Comparisons with experiment, where possible, also show good agreement.
Author | : J.R. Collingbourne |
Publisher | : |
Total Pages | : 15 |
Release | : 1964 |
Genre | : Pressure |
ISBN | : |
Download A Semi-emperical Prediction Method for Pressures on the Windward Surface of Circular Cones at Incidence at High Supersonic and Hypersonic Speeds(M>3) by J.R.Collingbourne, L.F.Crabtree and W.J.Bartlett Book in PDF, Epub and Kindle
Author | : C. C. Pappas |
Publisher | : |
Total Pages | : 28 |
Release | : 1972 |
Genre | : Aerodynamic heating |
ISBN | : |
Download Calculation of Laminar Heat Transfer to the Windward Surfaces of Straight Wing Shuttle Vehicles at High Angle of Attack and with Yaw Book in PDF, Epub and Kindle
Calculations of laminar heat transfer to windward wing and body surfaces of a straight wing MSC orbiter have been made at high angles of attack and with yaw. The predictions of heat transfer made by swept cylinder theory generally agree with measurements in areas free of external flow interference. An optimum elliptic cross section was then determined using swept cylinder theory for an aerodynamically heated windward body surface in radiation equilibrium.