Aerodynamic Heating and Thermal Protection Systems - download pdf or read online

By L. S. Fletcher

ISBN-10: 091592823X

ISBN-13: 9780915928231

Show description

Read or Download Aerodynamic Heating and Thermal Protection Systems PDF

Best aeronautics & astronautics books

Flight vehicle performance and aerodynamic control - download pdf or read online

Annotation "Flight automobile functionality and Aerodynamic keep an eye on is designed to function a textual content for both an 11-week or a 16-week direction on the sophomore point. It explains regular equipment used to estimate airplane functionality, the theoretical foundation of those tools, and the way a number of parameters derived from the airplane geometry can be utilized to estimate the necessities of keep an eye on surfaces and the aerodynamic forces required to actuate those surfaces.

Download e-book for kindle: Aircraft Stories: Decentering the Object in Technoscience by John Law

In airplane tales famous sociologist of technoscience John legislation tells “stories” a couple of British try to construct an army aircraft—the TSR2. The intertwining of those tales demonstrates the ways that specific technological initiatives might be understood in an international of advanced contexts. legislation works to dissatisfied the binary among the modernist proposal of information, topics, and items as having based and urban essences and the postmodernist proposal that each one is fragmented and centerless.

Additional info for Aerodynamic Heating and Thermal Protection Systems

Sample text

1971, pp. 122-130. 12 Zoby, E. V. , "Empirical Stagnation-Point Heat-Transfer Relation in Several Gas Mixtures at High Enthalpy Levels ," NASA TN D-l+799, 1968. Lees , L. , "Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds," Jet Propulsion, Vol. 26, April 1956, pp. 259-269. Libby, P. A . , June 1958. Marvin, J. G. and Derwert, G. S . , "Convective Heat Transfer in Planetary Gases," NASA TR R-22^, 1965. "Pioneer Venus," NASA TM X-62379, 1972. 17Moss, James N. , Zoby, E. Vincent, Sutton, Kenneth, and Anderson, E.

Sutton, K . , July 1973; also AIAA Journal, Vol. 12, Aug. 197^, pp. 1033-1105. Sutton, K. and Falanga, R. A . , "Stagnation Region Radiative Heating With Steady-State Ablation During Venus Entry," Journal of Spacecraft and Rockets, Vol. 10, Feb. 1973, pp. 155-157. ^Falanga, R. A. and Olstad, W. B. , July 197U. Brewer, R. A. , May 1975. 7 Moss, J. N . , Anderson, E. C . , a n d B o l z , C. W . , "Aerothermal Environment for Jovian Entry Probes," AIAA Progress in Astronautics and Aeronautics: Thermophysics of Spacecraft and Outer Planet Entry Probes , Vol.

Knowing m from the solution of Eqs. (7), (8), and (9), the discharge coefficient is obtained through Eq. (2). 34 SCOTT, MURRAY, AND MILHOAN Results and Discussion Two categories of experiments were performed on the test article in the supersonic duct. In the first category, a series of short experiments was conducted in which the external flow parameters and the seal gap width were varied to determine their effects on the internal heating in the test article. From these measurements, the internal heating rate could be correlated with environmental parameters.

Download PDF sample

Aerodynamic Heating and Thermal Protection Systems by L. S. Fletcher

by Charles

Rated 4.82 of 5 – based on 19 votes