skip to content
Prediction of Pressure Fluctuations Associated with Maneuvering Re-entry Weapons. Volume 1 Preview this item
ClosePreview this item
Checking...

Prediction of Pressure Fluctuations Associated with Maneuvering Re-entry Weapons. Volume 1

Author: Anthony L Laganelli; John R Howe; Air Force Flight Dynamics Laboratory (U.S.); General Electric Company. Re-entry and Environmental Systems Division.
Publisher: Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977.
Series: Technical report (Air Force Flight Dynamics Laboratory (U.S.)), AFFDL TR 77-59.
Edition/Format:   Print book : National government publication : English
Database:WorldCat
Summary:
An experimental program was conducted at the AEDC vonKarman facility, Tunnels A and B, in which acoustic pressure fluctuation data were acquired on a 7 degree half-cone-angle model featuring a control surface. The objective was to define the aeroacoustic environment applicable to re-entry vibration response analysis for both ballistic and maneuvering vehicles. Wind tunnel measurements were obtained at Mach 4 and 8  Read more...
Rating:

(not yet rated) 0 with reviews - Be the first.

Subjects
More like this

 

Find a copy in the library

&AllPage.SpinnerRetrieving; Finding libraries that hold this item...

Details

Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: Anthony L Laganelli; John R Howe; Air Force Flight Dynamics Laboratory (U.S.); General Electric Company. Re-entry and Environmental Systems Division.
OCLC Number: 422723280
Notes: "July 1977."
ADB023441 (from http://www.dtic.mil).
Research supported by the Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, and performed by General Electric Company, Re-entry and Environmental Systems Division.
Description: xvii, 224 pages : illustrations ; 28 cm.
Series Title: Technical report (Air Force Flight Dynamics Laboratory (U.S.)), AFFDL TR 77-59.
Responsibility: Anthony L. Laganelli, John R. Howe.

Abstract:

An experimental program was conducted at the AEDC vonKarman facility, Tunnels A and B, in which acoustic pressure fluctuation data were acquired on a 7 degree half-cone-angle model featuring a control surface. The objective was to define the aeroacoustic environment applicable to re-entry vibration response analysis for both ballistic and maneuvering vehicles. Wind tunnel measurements were obtained at Mach 4 and 8 for several values of freestream Reynolds number and model angle of attack. Stationary zones of laminar, transitional, and turbulent flow over the model were achieved. Acoustic data were reduced to rms fluctuating pressure, and power and cross-power spectral densities. Results were normalized using local boundary layer parameters for comparison with previous high speed measurements. The present study re-examined the aeroacoustic environment prediction capability relative to compressible flow conditions. Moreover, boundary layer characteristic lengths and velocities were reviewed in order to develop normalization procedures required for development of appropriate aeroacoustic scaling laws. It was determined that fluctuating pressure characteristics described by incompressible theory as well as empirical correlations could be modified to a compressible state through a transformation function. In this manner, compressible data were transformed to the incompressible plane where direct use of more tractable prediction techniques are available for engineering design analyses.

Reviews

User-contributed reviews
Retrieving GoodReads reviews...
Retrieving DOGObooks reviews...

Tags

Be the first.
Confirm this request

You may have already requested this item. Please select Ok if you would like to proceed with this request anyway.

Linked Data


Primary Entity

<http://www.worldcat.org/oclc/422723280> # Prediction of Pressure Fluctuations Associated with Maneuvering Re-entry Weapons. Volume 1
    a schema:CreativeWork, schema:Book ;
   library:oclcnum "422723280" ;
   library:placeOfPublication <http://experiment.worldcat.org/entity/work/data/137617196#Place/wright_patterson_air_force_base_ohio> ; # Wright-Patterson Air Force Base, Ohio
   library:placeOfPublication <http://id.loc.gov/vocabulary/countries/ohu> ;
   schema:about <http://id.worldcat.org/fast/1744047> ; # Wind tunnel testing
   schema:about <http://id.worldcat.org/fast/1127959> ; # Space vehicles--Atmospheric entry
   schema:about <http://id.worldcat.org/fast/991079> ; # Laminar flow
   schema:about <http://id.worldcat.org/fast/949009> ; # Guided missiles--Control systems
   schema:about <http://id.loc.gov/authorities/subjects/sh85125973> ; # Space vehicles--Atmospheric entry
   schema:about <http://id.loc.gov/authorities/subjects/sh85057727> ; # Guided missiles--Control systems
   schema:about <http://id.worldcat.org/fast/1159225> ; # Turbulent boundary layer
   schema:bookFormat bgn:PrintBook ;
   schema:contributor <http://viaf.org/viaf/157986428> ; # Air Force Flight Dynamics Laboratory (U.S.)
   schema:contributor <http://experiment.worldcat.org/entity/work/data/137617196#Person/howe_john_r> ; # John R. Howe
   schema:contributor <http://viaf.org/viaf/139657769> ; # General Electric Company. Re-entry and Environmental Systems Division.
   schema:creator <http://experiment.worldcat.org/entity/work/data/137617196#Person/laganelli_anthony_l> ; # Anthony L. Laganelli
   schema:datePublished "1977" ;
   schema:description "An experimental program was conducted at the AEDC vonKarman facility, Tunnels A and B, in which acoustic pressure fluctuation data were acquired on a 7 degree half-cone-angle model featuring a control surface. The objective was to define the aeroacoustic environment applicable to re-entry vibration response analysis for both ballistic and maneuvering vehicles. Wind tunnel measurements were obtained at Mach 4 and 8 for several values of freestream Reynolds number and model angle of attack. Stationary zones of laminar, transitional, and turbulent flow over the model were achieved. Acoustic data were reduced to rms fluctuating pressure, and power and cross-power spectral densities. Results were normalized using local boundary layer parameters for comparison with previous high speed measurements. The present study re-examined the aeroacoustic environment prediction capability relative to compressible flow conditions. Moreover, boundary layer characteristic lengths and velocities were reviewed in order to develop normalization procedures required for development of appropriate aeroacoustic scaling laws. It was determined that fluctuating pressure characteristics described by incompressible theory as well as empirical correlations could be modified to a compressible state through a transformation function. In this manner, compressible data were transformed to the incompressible plane where direct use of more tractable prediction techniques are available for engineering design analyses."@en ;
   schema:exampleOfWork <http://worldcat.org/entity/work/id/137617196> ;
   schema:genre "National government publication"@en ;
   schema:genre "Government publication"@en ;
   schema:inLanguage "en" ;
   schema:isPartOf <http://experiment.worldcat.org/entity/work/data/137617196#Series/technical_report_air_force_flight_dynamics_laboratory_u_s> ; # Technical report (Air Force Flight Dynamics Laboratory (U.S.)) ;
   schema:isPartOf <http://experiment.worldcat.org/entity/work/data/137617196#Series/air_force_flight_dynamics_laboratory_u_s_technical_report> ; # Air Force Flight Dynamics Laboratory (U.S.). Technical report ;
   schema:name "Prediction of Pressure Fluctuations Associated with Maneuvering Re-entry Weapons. Volume 1"@en ;
   schema:productID "422723280" ;
   schema:publication <http://www.worldcat.org/title/-/oclc/422723280#PublicationEvent/wright_patterson_air_force_base_ohio_air_force_flight_dynamics_laboratory_air_force_wright_aeronautical_laboratories_air_force_systems_command_united_states_air_force_1977> ;
   schema:publisher <http://experiment.worldcat.org/entity/work/data/137617196#Agent/air_force_flight_dynamics_laboratory_air_force_wright_aeronautical_laboratories_air_force_systems_command_united_states_air_force> ; # Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force
   wdrs:describedby <http://www.worldcat.org/title/-/oclc/422723280> ;
    .


Related Entities

<http://experiment.worldcat.org/entity/work/data/137617196#Agent/air_force_flight_dynamics_laboratory_air_force_wright_aeronautical_laboratories_air_force_systems_command_united_states_air_force> # Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force
    a bgn:Agent ;
   schema:name "Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force" ;
    .

<http://experiment.worldcat.org/entity/work/data/137617196#Person/howe_john_r> # John R. Howe
    a schema:Person ;
   schema:familyName "Howe" ;
   schema:givenName "John R." ;
   schema:name "John R. Howe" ;
    .

<http://experiment.worldcat.org/entity/work/data/137617196#Person/laganelli_anthony_l> # Anthony L. Laganelli
    a schema:Person ;
   schema:familyName "Laganelli" ;
   schema:givenName "Anthony L." ;
   schema:name "Anthony L. Laganelli" ;
    .

<http://experiment.worldcat.org/entity/work/data/137617196#Place/wright_patterson_air_force_base_ohio> # Wright-Patterson Air Force Base, Ohio
    a schema:Place ;
   schema:name "Wright-Patterson Air Force Base, Ohio" ;
    .

<http://experiment.worldcat.org/entity/work/data/137617196#Series/air_force_flight_dynamics_laboratory_u_s_technical_report> # Air Force Flight Dynamics Laboratory (U.S.). Technical report ;
    a bgn:PublicationSeries ;
   schema:hasPart <http://www.worldcat.org/oclc/422723280> ; # Prediction of Pressure Fluctuations Associated with Maneuvering Re-entry Weapons. Volume 1
   schema:name "Air Force Flight Dynamics Laboratory (U.S.). Technical report ;" ;
    .

<http://experiment.worldcat.org/entity/work/data/137617196#Series/technical_report_air_force_flight_dynamics_laboratory_u_s> # Technical report (Air Force Flight Dynamics Laboratory (U.S.)) ;
    a bgn:PublicationSeries ;
   schema:hasPart <http://www.worldcat.org/oclc/422723280> ; # Prediction of Pressure Fluctuations Associated with Maneuvering Re-entry Weapons. Volume 1
   schema:name "Technical report (Air Force Flight Dynamics Laboratory (U.S.)) ;" ;
    .

<http://id.loc.gov/authorities/subjects/sh85057727> # Guided missiles--Control systems
    a schema:Intangible ;
   schema:name "Guided missiles--Control systems"@en ;
    .

<http://id.loc.gov/authorities/subjects/sh85125973> # Space vehicles--Atmospheric entry
    a schema:Intangible ;
   schema:name "Space vehicles--Atmospheric entry"@en ;
    .

<http://id.worldcat.org/fast/1127959> # Space vehicles--Atmospheric entry
    a schema:Intangible ;
   schema:name "Space vehicles--Atmospheric entry"@en ;
    .

<http://id.worldcat.org/fast/1159225> # Turbulent boundary layer
    a schema:Intangible ;
   schema:name "Turbulent boundary layer"@en ;
    .

<http://id.worldcat.org/fast/1744047> # Wind tunnel testing
    a schema:Intangible ;
   schema:name "Wind tunnel testing"@en ;
    .

<http://id.worldcat.org/fast/949009> # Guided missiles--Control systems
    a schema:Intangible ;
   schema:name "Guided missiles--Control systems"@en ;
    .

<http://id.worldcat.org/fast/991079> # Laminar flow
    a schema:Intangible ;
   schema:name "Laminar flow"@en ;
    .

<http://viaf.org/viaf/139657769> # General Electric Company. Re-entry and Environmental Systems Division.
    a schema:Organization ;
   schema:name "General Electric Company. Re-entry and Environmental Systems Division." ;
    .

<http://viaf.org/viaf/157986428> # Air Force Flight Dynamics Laboratory (U.S.)
    a schema:Organization ;
   schema:name "Air Force Flight Dynamics Laboratory (U.S.)" ;
    .

<http://www.worldcat.org/title/-/oclc/422723280>
    a genont:InformationResource, genont:ContentTypeGenericResource ;
   schema:about <http://www.worldcat.org/oclc/422723280> ; # Prediction of Pressure Fluctuations Associated with Maneuvering Re-entry Weapons. Volume 1
   schema:dateModified "2016-05-11" ;
   void:inDataset <http://purl.oclc.org/dataset/WorldCat> ;
    .

<http://www.worldcat.org/title/-/oclc/422723280#PublicationEvent/wright_patterson_air_force_base_ohio_air_force_flight_dynamics_laboratory_air_force_wright_aeronautical_laboratories_air_force_systems_command_united_states_air_force_1977>
    a schema:PublicationEvent ;
   schema:location <http://experiment.worldcat.org/entity/work/data/137617196#Place/wright_patterson_air_force_base_ohio> ; # Wright-Patterson Air Force Base, Ohio
   schema:organizer <http://experiment.worldcat.org/entity/work/data/137617196#Agent/air_force_flight_dynamics_laboratory_air_force_wright_aeronautical_laboratories_air_force_systems_command_united_states_air_force> ; # Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force
   schema:startDate "1977" ;
    .


Content-negotiable representations

Close Window

Please sign in to WorldCat 

Don't have an account? You can easily create a free account.