Explore: Transonic Planes
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AI-Generated Overview About “transonic-planes”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
By Milton Lamb
“Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Metadata:
- Title: ➤ Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
- Author: Milton Lamb
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va
“Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Subjects and Themes:
- Subjects: ➤ Statistics - Testing - Laminar flow - Turbulent flow - Pylons - Wing nacelle configurations - Wind tunnel tests - Airplanes - Transonic planes - Nacelles - Wings - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL18217665M - OL18468463M - OL17724275M
- Online Computer Library Center (OCLC) ID: 776151030
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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2A study of canard-wing interference using experimental pressure data at transonic speeds
By Blair B. Gloss
“A study of canard-wing interference using experimental pressure data at transonic speeds” Metadata:
- Title: ➤ A study of canard-wing interference using experimental pressure data at transonic speeds
- Author: Blair B. Gloss
- Language: English
- Number of Pages: Median: 68
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1979
- Publish Location: [Washington] - Springfield, Va
“A study of canard-wing interference using experimental pressure data at transonic speeds” Subjects and Themes:
- Subjects: Airplanes - Canard Wings - Transonic planes - Wings - Wings, Canard
Edition Identifiers:
- The Open Library ID: OL18014499M - OL15229385M - OL17538400M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Flight-determined stability and control derivatives for the F-111 TACT research aircraft
By Alex G. Sim
“Flight-determined stability and control derivatives for the F-111 TACT research aircraft” Metadata:
- Title: ➤ Flight-determined stability and control derivatives for the F-111 TACT research aircraft
- Author: Alex G. Sim
- Language: English
- Number of Pages: Median: 76
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Service
- Publish Date: 1978
- Publish Location: Springfield, Va - [Washington]
“Flight-determined stability and control derivatives for the F-111 TACT research aircraft” Subjects and Themes:
- Subjects: Wings - Transonic planes - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL15229380M - OL17538394M - OL18014495M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4A grid-embedding transonic flow analysis computer program for wing/nacelle configurations
By Essam H. Atta
“A grid-embedding transonic flow analysis computer program for wing/nacelle configurations” Metadata:
- Title: ➤ A grid-embedding transonic flow analysis computer program for wing/nacelle configurations
- Author: Essam H. Atta
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1983
- Publish Location: Moffett Field, Calif
“A grid-embedding transonic flow analysis computer program for wing/nacelle configurations” Subjects and Themes:
- Subjects: Airplanes - Transonic planes - Nacelles
Edition Identifiers:
- The Open Library ID: OL18038220M - OL17555792M - OL15310341M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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5Fast euler solver for steady one-dimensional flows
By Gino Moretti
“Fast euler solver for steady one-dimensional flows” Metadata:
- Title: ➤ Fast euler solver for steady one-dimensional flows
- Author: Gino Moretti
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ NASA Scientific and Technical Information Branch - National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1983
- Publish Location: ➤ [s.l.] - [Springfield, Va - Washington, D.C
“Fast euler solver for steady one-dimensional flows” Subjects and Themes:
- Subjects: Euler's numbers - One-dimensional flow - Transonic planes
Edition Identifiers:
- The Open Library ID: OL15304194M - OL13839404M - OL17829858M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6EUROSHOCK
By Egon Stanewsky, Jean Delery, John Fulker and Wolfgang Geissler
“EUROSHOCK” Metadata:
- Title: EUROSHOCK
- Authors: Egon StanewskyJean DeleryJohn FulkerWolfgang Geissler
- Language: English
- Number of Pages: Median: 414
- Publisher: ➤ Vieweg - Friedrich Vieweg & Sohn Verlag
- Publish Date: 1997
- Publish Location: Braunschweig/Wiesbaden
“EUROSHOCK” Subjects and Themes:
- Subjects: ➤ Shock waves - Drag (Aerodynamics) - Boundary layer control - Transonic planes - Research - Wings - Design and construction
- Places: European Union countries
Edition Identifiers:
- The Open Library ID: OL12768781M - OL20954927M
- All ISBNs: 3528076569 - 9783528076566
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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7A study of canard-wing interference using experimental pressure data at transonic speeds
By Blair B Gloss
“A study of canard-wing interference using experimental pressure data at transonic speeds” Metadata:
- Title: ➤ A study of canard-wing interference using experimental pressure data at transonic speeds
- Author: Blair B Gloss
- Language: English
- Number of Pages: Median: 68
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1979
- Publish Location: [Washington] - Springfield, Va
“A study of canard-wing interference using experimental pressure data at transonic speeds” Subjects and Themes:
- Subjects: Airplanes - Canard Wings - Transonic planes - Wings - Wings, Canard
Edition Identifiers:
- The Open Library ID: OL14932253M - OL17979155M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Flight-determined stability and control derivatives for the F-111 TACT research aircraft
By Alex G Sim
“Flight-determined stability and control derivatives for the F-111 TACT research aircraft” Metadata:
- Title: ➤ Flight-determined stability and control derivatives for the F-111 TACT research aircraft
- Author: Alex G Sim
- Language: English
- Number of Pages: Median: 76
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Service - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: [Washington] - Springfield, Va
“Flight-determined stability and control derivatives for the F-111 TACT research aircraft” Subjects and Themes:
- Subjects: Handling characteristics - Airplanes - Wings - Transonic planes - Stability of airplanes
Edition Identifiers:
- The Open Library ID: OL14932246M - OL17979143M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
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9Wave drag as the objective function in transonic fighter wing optimization
By Pamela S. Phillips
“Wave drag as the objective function in transonic fighter wing optimization” Metadata:
- Title: ➤ Wave drag as the objective function in transonic fighter wing optimization
- Author: Pamela S. Phillips
- Language: English
- Number of Pages: Median: 20
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Wave drag as the objective function in transonic fighter wing optimization” Subjects and Themes:
- Subjects: Wings - Design and construction - Transonic planes - Wave mechanics - Fighter planes
Edition Identifiers:
- The Open Library ID: OL17830296M - OL17663543M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10TAS--a transport aircraft/store flow field prediction code
By D. S. Thompson
“TAS--a transport aircraft/store flow field prediction code” Metadata:
- Title: ➤ TAS--a transport aircraft/store flow field prediction code
- Author: D. S. Thompson
- Language: English
- Number of Pages: Median: 50
- Publisher: ➤ The Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“TAS--a transport aircraft/store flow field prediction code” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Transonic Aerodynamics - Transonic planes
Edition Identifiers:
- The Open Library ID: OL18036927M - OL17663525M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
By Francis J Capone
“Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft” Metadata:
- Title: ➤ Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft
- Author: Francis J Capone
- Language: English
- Number of Pages: Median: 334
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effects of varying podded nacelle-nozzle installations on transonic aeropropulsive characteristics of a supersonic fighter aircraft” Subjects and Themes:
- Subjects: ➤ Airplanes - Canard Wings - Nacelles - Supersonic planes - Transonic planes - Wings, Canard
Edition Identifiers:
- The Open Library ID: OL14933304M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Buffet characteristics of the F-8 supercritical wing airplane
By V. Michael DeAngelis
“Buffet characteristics of the F-8 supercritical wing airplane” Metadata:
- Title: ➤ Buffet characteristics of the F-8 supercritical wing airplane
- Author: V. Michael DeAngelis
- Language: English
- Number of Pages: Median: 29
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1977
- Publish Location: [Washington] - Springfield, Va
“Buffet characteristics of the F-8 supercritical wing airplane” Subjects and Themes:
- Subjects: Transonic planes - Wind tunnels - Buffeting (Aerodynamics) - Flow visualization - Wings
Edition Identifiers:
- The Open Library ID: OL14925140M
Author's Alternative Names:
"V Michael DeAngelis"Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Wing analysis using a transonic potential flow computational method
By P. A Henne
“Wing analysis using a transonic potential flow computational method” Metadata:
- Title: ➤ Wing analysis using a transonic potential flow computational method
- Author: P. A Henne
- Language: English
- Number of Pages: Median: 55
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: [Washington] - Springfield, Va
“Wing analysis using a transonic potential flow computational method” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Mathematical models - Transonic Aerodynamics - Transonic planes - Wings
Edition Identifiers:
- The Open Library ID: OL14925453M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
By Milton Lamb
“Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Metadata:
- Title: ➤ Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
- Author: Milton Lamb
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Subjects and Themes:
- Subjects: ➤ Nacelles - Skin friction - Pylons - System effectiveness - Wind tunnel tests - Testing - Airplanes - Aerodynamic drag - Transonic planes - Wings
Edition Identifiers:
- The Open Library ID: OL16152786M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15Numerical optimization design of advanced transonic wing configurations
By Gary B Cosentino
“Numerical optimization design of advanced transonic wing configurations” Metadata:
- Title: ➤ Numerical optimization design of advanced transonic wing configurations
- Author: Gary B Cosentino
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1984
- Publish Location: Moffett Field, Calif
“Numerical optimization design of advanced transonic wing configurations” Subjects and Themes:
- Subjects: Wings - Transonic planes
Edition Identifiers:
- The Open Library ID: OL14926478M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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16Effect of a variable camber and twist wing at transonic mach numbers
By James C Ferris
“Effect of a variable camber and twist wing at transonic mach numbers” Metadata:
- Title: ➤ Effect of a variable camber and twist wing at transonic mach numbers
- Author: James C Ferris
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1984
- Publish Location: [Washington, D.C.?]
“Effect of a variable camber and twist wing at transonic mach numbers” Subjects and Themes:
- Subjects: Testing - Wings - Transonic planes
Edition Identifiers:
- The Open Library ID: OL14926734M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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17TAS
By D. S Thompson
“TAS” Metadata:
- Title: TAS
- Author: D. S Thompson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1983
- Publish Location: [Washington, D.C.]
“TAS” Subjects and Themes:
- Subjects: Transonic wind tunnels - Testing - Transonic planes
Edition Identifiers:
- The Open Library ID: OL14931238M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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18Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane
By Edward L Friend
“Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane” Metadata:
- Title: ➤ Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane
- Author: Edward L Friend
- Language: English
- Number of Pages: Median: 75
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - [Washington]
“Flight comparison of the transonic agility of the F-111A airplane and the F-111 supercritical wing airplane” Subjects and Themes:
- Subjects: F-111 (Jet fighter plane) - Wings - Transonic planes
Edition Identifiers:
- The Open Library ID: OL14932267M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Wave drag as the objective function in transonic fighter wing optimization
By Pamela S Phillips
“Wave drag as the objective function in transonic fighter wing optimization” Metadata:
- Title: ➤ Wave drag as the objective function in transonic fighter wing optimization
- Author: Pamela S Phillips
- Language: English
- Number of Pages: Median: 20
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1984
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Wave drag as the objective function in transonic fighter wing optimization” Subjects and Themes:
- Subjects: Wings - Design and construction - Transonic planes - Wave mechanics - Fighter planes
Edition Identifiers:
- The Open Library ID: OL14933508M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Transonic airfoil design using cartesian coordinates
By Leland A. Carlson
“Transonic airfoil design using cartesian coordinates” Metadata:
- Title: ➤ Transonic airfoil design using cartesian coordinates
- Author: Leland A. Carlson
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ U.S. National Aeronautics and Space Administration - for sale by the National Technical Information Service
- Publish Date: 1976
- Publish Location: Washington - Springfield, Va
“Transonic airfoil design using cartesian coordinates” Subjects and Themes:
- Subjects: Aerofoils - Transonic planes - Design and construction
Edition Identifiers:
- The Open Library ID: OL15208716M
Access and General Info:
- First Year Published: 1976
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Transonic
Transonic (or transsonic) flow is air flowing around an object at a speed that generates regions of both subsonic and supersonic airflow around that object
List of X-planes
have also since sponsored X-plane projects. The first experimental aircraft specification, for a transonic rocket plane, was placed in 1945, and the
Airplane
that of smaller private planes, with the per-mile statistic indicating that airliners are 8.3 times safer than smaller planes. Like all activities involving
Swept wing
Wings: Convair's High-Speed Planes of the Fifties and Sixties. Motorbooks. 1983. Myhra, David. Focke-Wulf Ta 183 (X Planes of the Third Reich). Atglen
Area rule
Whitcomb and also called the transonic area rule, is a design procedure used to reduce an aircraft's drag at transonic speeds which occur between about
Sound barrier
reliable in the transonic. Further, a series of tests made by Karl Doetsch at the behest of Willy Messerschmitt found that the plane became uncontrollable
Tailplane
tail planes of the old Farman biplanes were "lifting tail planes," and were, as a matter of fact, rather heavily cambered. By a non-lifting tail plane is
Boeing X-66
11 ft (3.4 m) transonic tunnel, then later in 2019 at the 14 by 22 ft (4.3 by 6.7 m) subsonic tunnel at NASA Langley. A full-scale X-plane is being developed
Boeing Truss-Braced Wing
"NASA Picks Boeing's Transonic Truss-Based Wing For Sustainable X-Plane". Aviation Week. "Boeing producing battery-powered hybrid plane". Northwest Cable
Mach number
categories:[citation needed] At transonic speeds, the flow field around the object includes both sub- and supersonic parts. The transonic period begins when first