Aircraft Performance and Design by Anderson

By Anderson

Written through the most capable aerospace authors, this new publication develops plane functionality recommendations from first rules and applies then to actual airplanes. It additionally tackle a philosophy of, and methods for airplane layout. via constructing and discussing those topics in one textual content, the writer captures a level of synergism no longer present in different texts. The ebook is written in a conversational sort, an indicator of all of john anderson's texts, to augment the readers' realizing.

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17) where Z e is the compressibility factor, and approximately equals 1 if the real gas effects are insignificant. After simplification and comparison, it is shown Wr ∝ 1/K 2 . In the engineering practice, K 2 has been widely used to normalize and to compare various experimental and numerical data [10–14], and fitted formulas based on K 2 have extended the scope of application to flows in the near free molecular flow regime. 4 demonstrates the variation trend of the stagnation point heat transfer coefficients of spherically blunted cones with different nose radii under various incoming free stream conditions.

Rosner DE (1963) Scale effects and correlations in non-equilibrium convective heat transfer. AIAA J 1:1550–1555 87. Voronkin VG (1971) Non-equilibrium viscous flow of a multicomponent gas in the vicinity of the stagnation point of a blunt body. Fluid Dyn 6(2):308–311 88. Serpico M, Monti R, Savino R (1998) Heat flux on partially catalytic surfaces in hypersonic flows. J Spacecraft Rockets 35:9–15 89. Gokcen Tahir (1996) Effects of freestream non-equilibrium on convective heat transfer to a blunt body.

Oran ES, Oh CK, Cybyk BZ (1998) Direct simulation Monte Carlo: recent advances and applications. Annu Rev Fluid Mech 1998(30):403441 47. Aktas O, Aluru NR (2002) A combined continuum/DSMC technique for multiscale analysis of microfluidic filters. J Comput Phys 178(2):342–372 48. Wijesinghe HS (2003) Hybrid atomistic-continuum formulations for gaseous flows. D. thesis, Massachusetts Institute of Technology 49. Wang W-L (2004) A hybrid particle/continuum approach for non-equilibrium hypersonic flows.

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