Last edited by Brazragore
Wednesday, April 15, 2020 | History

2 edition of study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14 found in the catalog.

study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14

Harry W. Carlson

study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14

  • 246 Want to read
  • 22 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Technical Information Service in [Washington], Springfield Va .
Written in English

    Subjects:
  • Sonic boom.,
  • Space vehicles -- Testing.,
  • Aerodynamics, Supersonic.

  • Edition Notes

    StatementHarry W. Carlson and Robert J. Mack ; NASA Langley Research Center.
    SeriesNASA technical paper ; 1015, NASA technical paper -- 1015.
    ContributionsMack, Robert J., Langley Research Center., United States. National Aeronautics and Space Administration.
    The Physical Object
    Pagination[1], 28, [1] p. :
    Number of Pages28
    ID Numbers
    Open LibraryOL18012757M


Share this book
You might also like
Francis Bacon, recent paintings

Francis Bacon, recent paintings

Property report of the Secretary of the Senate. Letter from the Secretary of the Senate transmitting in obedience to law an account of all property, including stationery, belonging to the United States in his possession on the 3d day of December, 1917.

Property report of the Secretary of the Senate. Letter from the Secretary of the Senate transmitting in obedience to law an account of all property, including stationery, belonging to the United States in his possession on the 3d day of December, 1917.

The industrialization of Europe; 1780-1914

The industrialization of Europe; 1780-1914

Anybody can learn to play the piano

Anybody can learn to play the piano

Cracking the AP Spanish exam

Cracking the AP Spanish exam

Yupʼik Eskimo dictionary

Yupʼik Eskimo dictionary

Basic principles of classical ballet

Basic principles of classical ballet

Daily observations, or, Meditations divine, morall

Daily observations, or, Meditations divine, morall

Bible records, Barbour County, Alabama

Bible records, Barbour County, Alabama

Basic training in nutrition.

Basic training in nutrition.

Geology of Marion County, Indiana

Geology of Marion County, Indiana

Atgets Seven Albums (Yale Publications in the History of Art)

Atgets Seven Albums (Yale Publications in the History of Art)

Y cwtta cyfarwydd

Y cwtta cyfarwydd

Collecting Matisse

Collecting Matisse

Hearing on corporate tax reform

Hearing on corporate tax reform

study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14 by Harry W. Carlson Download PDF EPUB FB2

Study of the sonic-boom characteristics of a blunt body at a Mach number of [Washington]: National Aeronautics and Space Administration, Scientific and. Effect of a variable-geometry diffuser on the operating characteristics of a helium tunnel designed for a mach number in excess of 20 / (Washington, [D.C.]: National Aeronautics and Space Administration, ), by Patrick J.

Johnston, Robert D. Witcofski, and Langley Research Center (page images at. Red dotted and black dot-dashed vertical lines denote the critical Mach number for BR = andrespectively.

(a) Total, pressure, and friction drag for BR = and and (b) ratio of. Whether you've loved the book or not, if you give your honest and detailed thoughts then people will find new books that are right for them. 1 Texto y sociedad en las letras francesas y francófonas: XVI Coloquio de la Asociación de Profesores de Francés de la Universidad Española (APFUE), celebrado del 25 al 27 de abril de en Lleida.

The book is designed to talk to the reader; in part to be a self-teaching instrument. Learning objectives have been added to each chapter to reflect what is believed to be the most important items to learn from that particular chapter.

mach number aerodynamics compressible flow dimensional vortex finite tunnel. Full text of "NASA scientific and technical publications: A catalog of Special Publications, Reference Publications, Conference Publications, and Technical Papers, " See other formats. Get this from a library. Fundamentals of aerodynamics.

[John D Anderson, Jr.] -- Offering an up-to-date overview of the field of aerodynamics, this edition covers many of the key concepts and topics, such as linearized supersonic flow and oblique shock and expansion waves.

Formulation of the problem of sonic boom by a maneuvering aerofoil as a one-parameter family of Cauchy problems. is the mean of the Mach number m on the nonlinear wavefront just behind. Typical aspect ratios structural of In order to appreciate the effect the planform vary sail- performance high a for 33 from neces- on the aerodynamic characteristics, it is to plane a for to for a jet fighter to which manner in the wing a study sary saucer.

flying Figure illustrates the three. Full text of "Fundamentals Of Aerodynamics, 6th Edition" See other formats. This banner text can have markup. web; books; video; audio; software; images; Toggle navigation.

(a) 著書・雑誌論文 T. Nagata, A. Noguchi, T. Nonomura, K. Ohtani, K. Asai, "Experimental investigation of transonic and supersonic flow over a sphere for Reynolds numbers of 10 5 by free‐flight tests with schlieren visualization", Shock Waves, vol(2), pp ().>>abstract Y.

Uwamino, M. Fujiwara, H. Tomizaki, K. Ohtani, K. Makihara, "Damage of twisted tape tethers. Moreover, virtually every full ray trace sonic boom program in use today is evolved in one way or another from one of these two programs.”20 In Juneat the end of the AST program’s first year, Harry Carlson, Raymond Barger, and Robert Mack of the Langley Research Center published a study on the applicability of sonic boom minimization.

Full text of "Jet Engine Fundamental Of Theory Design Operations" See other formats. Also, wing angle of attack is Q while section angle of attack is differentiated by the use of 01~. The study of section properties allows an objective consideration of the effects of camber, thickness, etc.

The lift characteristics of five illustrative airfoil sections are shown in figure This book emphasizes that the aircraft design process is a science and an art, but also a compromise.

The authors address the conceptual design phase comprehensively, for both civil and military aircraft, from initial consideration of user needs, material selection, and structural arrangement to the decision to iterate the design one more time.

Holy Cross Catholic Church Jox's Podcast Sell Yourself Online Podcast with Jane Copeland Philosophy and Fun of Algebra In The Secret Place Gettin' Steamy with John Panini: A Gentleman's Guide to Success in Cooking, Love, and Body Grooming Central Texas Conference.

Confessions of a Serial Philosopher Coup Critique Podcast Body Language: The Yogis of India and Nepal Accept The Mystery podcast_between-panels_ Alexander Books - Lafayette, LA Blood Sweat & Tears Podcast. Full text of "DTIC ADA The Shock and Vibration Digest.

Volume 9. He was Number 1 Newfoundland, all systems, in andNumber 2 Working Dog and Number 8 All-breed in In addition to Josh, the Helmings have had many Newfs who have significantly.

D CONTENTS. 6 Editorial 10 Angel On A Leash 14 Brace Yourself. Look At 26 A William F. Stifel AKC PRESIDENT By Karl M. Stearns Hereís An Insightful Look At One Of AKCís And. The effects of compressibility at speeds approaching the critical Mach number on the performance of an aircraft are discussed at length in Chapter 11 dealing with high-speed flight.

The basic problem is that, if the air over any part of the aircraft structure (usually the wing) reaches the speed of sound there is an excessive rise in drag. Compare the specific excess power for a 10,lbf TA cruising at the Mach number required for while operating at "Mit" thrust with that for the aircraft cruising at a Mach number of and with that for the aircraft cruising at a Mach number of Nitrogen is often used in wind tunnels as the test gas substitute for air.

The primary purpose of sweepback is to increase the value of the critical Mach number for a given aircraft. The effects of compressibility at speeds approaching the critical Mach number on the performance of an aircraft are discussed at length in Chapter 11 dealing with high-speed flight.

The first f annual report included seven reports. courses capable of application to aeronautics, but only as follows: the Mfassachusetts Institute of Technology an d tlie No. Mach numbers are named after him and are the ratio of the speed of a body or fluid to the local speed of sound, Mach 1 refers to local speed.

When the ‘barrier’ is broken by a flying object (usually an aircraft) it moves from subsonic to supersonic speed and creates a sonic boom. Publishing platform for digital magazines, interactive publications and online catalogs.

Convert documents to beautiful publications and share them worldwide. Title: Computational fluid dynamics, Author: Maximiliano Alegre, Length: pages, Published: Researchers at Langley con-ducted generic and exploratory studies of the stability and control characteristics of this type of configura-tion in several wind tunnels, beginning in with an exploratory conventional static force-test study of variable-sweep version of the X-1 research airplane in the Langley mph 7- by Foot Tunnel In 5/5(2).

Bibio - Mind Bokeh () Dirty Beaches – Badlands () I’m pretty annoyed with ordinal reviews, or track-by-track enumerations that yield scores of for OK Computer, but I find myself slipping into that when I basically like everything about an album—and especially, as in the case of Badlands, when it feels like there’s so little to even mention.

PARD researchers calculated that this vehicle attained a speed of Mach 4_) As Wallops gained experience with its new boosters, the engineers began obtaining valuable data on the flight characteristics of objects moving at re-entry velocities.

Raw speed, of. Free essays, homework help, flashcards, research papers, book reports, term papers, history, science, politics. Supersonic Aircraft Optimization for Minimizing Drag and Sonic Boom A DISSERTATION SUBMITTED TO THE DEPARTMENT OF AERONAUTICS AND ASTRONAUTICS AND THE COMMITTEE ON GRADUATE STUDIES OF STANFORD UNIVERSITY IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY Martin K.

Chan August Physics of Music Science and Art Warren F. Rogers Westmont College, Santa Barbara CA To all my students, through all the years at Westmont College, especially to those who have taken, or are currently taking, the Physics of Music, this book is dedicated to you.

38 The Art of the Helicopter Fig. A body following a circular path is at constant acceleration and if this is calculated, it can be used to derive the forces acting.

(a) shows that after a short time δT, the velocity has changed direction. (b) The rate of change of velocity is the acceleration. Figure Reynolds number/Mach number correlations as a function of velocity and altitude for U.S.

Standard Atmosphere. The corresponding Reynolds number is ( x iO-4 /-too lbf.s2\/ ft4 x ft2 = x i07 CONCEPT OF THE BOUNDARY LAYER For many high-Reynolds-number flows (such as those of interest to the aerodynamicist).

Although the Mach number based on the speed of the complete aircraft may be low, in some cases, significant compressibility effects may be present on components of the vehicle. For example, flow over the upper surface of a wing with a thick high-lift airfoil at high angles of attack may experience Mach numbers approaching 1, even though the.

The Lifting Body Program falls into the category of a low cost, partial technology demonstration to reduce the high technical risk that was emerging from the Dyna Soar program (discussed in Chapter 2).

Notice that the Lifting Body Program was created PRIOR to cancellation of Dyna Soar, and was NOT a result of that cancellation. Special Powers Squared. When a number has a power of 2, it is commonly referred to as “squared.” For example, 72 is read as “seven squared” or “seven to the second power.” To remember this, think about how a square has two dimensions: length and width.

Cubed. When a number has a power of 3, it is commonly referred to as “cubed.”. Effective sound velocity and characteristic velocity as a function of altitude out of the entry plane.

Instantaneous energy release calculations as a function of meteor diameter, meteor mach number and horizontal entry angle evaluated for 1 km path intervals. Report from Committee on Banking and Currency to accompany S.

Nov. 7, 4 p. Study of Federal financial assistance to victims of flood disasters. Report from Committee on Banking and Currency to accompany S. Nov. 7, 19C3. 6 p. Providing for study of scenic and recreational highways by Committee on Public Works.

In ordering a publication from the Superintendent of Documents, giTe (if known) the name of the publishing department, bureau, or agency, and the title, together with the classification number which Is added to the entry at the ex- treme right ; order the congressional documents and reports by the title, together with the document or report.

) t Y 3. At 7: 34 Se 1/ AVIATION MEDICINE OFFICE, Federal Aviation Agency Washington, D.C. Aviation medical report AM (series). 66— Evaluation of head and face potential of current airline seats dur- ing crash decelerations [with list of references ; by] John J.

Swear- ingen. June [4] +14+ [2] p. Маршрут для велосипедистов будет действовать только в праздничные и выходные дни, о чём говорят информационные таблички, размещённые под знаком велосипедной полосы.The University of Sydney Calendar Volume II G —1 K PRINTED AND PUBLISHED IN AUSTRALIA BY VICTOR C.

N. BUGHT, GOVERNMENT PRINTER Contents In the Calendar.