1.

Record Nr.

UNINA9910462516803321

Autore

Pfanzagl J (Johann)

Titolo

Parametric statistical theory [[electronic resource] /] / Johann Pfanzagl, with the assistance of R. Hamböker

Pubbl/distr/stampa

Berlin ; ; New York, : W. de Gruyter, 1994

ISBN

3-11-088976-5

Edizione

[Reprint 2011]

Descrizione fisica

1 online resource (388 p.)

Collana

De Gruyter Textbook

Altri autori (Persone)

HambökerR

Disciplina

519.5/4

Soggetti

Mathematical statistics

Mathematics

Electronic books.

Lingua di pubblicazione

Inglese

Formato

Materiale a stampa

Livello bibliografico

Monografia

Note generali

Description based upon print version of record.

Nota di bibliografia

Includes bibliographical references (p. [345]-359) and indexes.

Nota di contenuto

Front matter -- Chapter 1 Sufficiency and completeness -- Chapter 2 The evaluation of estimators -- Chapter 3 Mean unbiased estimators and convex loss functions -- Chapter 4 Testing hypotheses -- Chapter 5 Confidence procedures -- Chapter 6 Consistent estimators -- Chapter 7 Asymptotic distributions of estimator sequences -- Chapter 8 Asymptotic bounds for the concentration of estimators and confidence bounds -- Chapter 9 Miscellaneous results on asymptotic distributions -- Chapter 10 Asymptotic test theory -- References -- Author Index -- Subject Index -- Notation Index

Sommario/riassunto

Parametric Statistical Theory



2.

Record Nr.

UNINA9910716562003321

Autore

Keyes J. Wayne

Titolo

Analytical and experimental studies of shock interference heating in hypersonic flows / / by J. Wayne Keyes and Frank D. Hains

Pubbl/distr/stampa

Washington, D.C. : , : National Aeronautics and Space Administration, , May 1973

Descrizione fisica

1 online resource (iv, 137 pages) : illustrations

Collana

NASA/TN ; ; D-7139

Soggetti

Fluid mechanics

Shock waves

Aerodynamic heating

Aerodynamics, Hypersonic

Boundary layer

Lingua di pubblicazione

Inglese

Formato

Materiale a stampa

Livello bibliografico

Monografia

Note generali

"May 1973."

Nota di bibliografia

Includes bibliographical references (pages 34-39).

Sommario/riassunto

An analytical and experimental study is presented of the aerodynamic heating resulting from six types of shock interference patterns encountered in high speed flow. Centerline measurements of pressure and heat transfer distributions on basic bodies were obtained in four wind tunnels for Mach numbers from 6 to 20, specific heat ratios from 1.27 to 1.67, and free stream Reynolds numbers from 3 million to 25.6 million per meter. Peak heating and peak pressures up to 17 and 7.5 times stagnation values, respectively, were measured. In general, results obtained from semiempirical methods developed for each of the six types of interference agreed with the experimental peaks.