Forebodies

40 books
Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5Peter F. Covell
⏱ 2h 53m

Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5

Peter F. Covell

1992173 pp.
A computational examination of directional stability for smooth and chined forebodies at high-aRamakrishnan Ravi
⏱ 1h 20m

A computational examination of directional stability for smooth and chined forebodies at high-a

Ramakrishnan Ravi

199280 pp.
F/A-18 forebody vortex controlBrian R. Kramer

F/A-18 forebody vortex control

Brian R. Kramer

1994No page data
Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attackBrent R. Cobleigh

Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack

Brent R. Cobleigh

2001No page data
Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slipRaymond D. Whipple
⏱ 4h 46m

Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip

Raymond D. Whipple

1986286 pp.
Flush airdata sensing (FADS) system calibration procedures and results for blunt forebodiesUnknown Author

Flush airdata sensing (FADS) system calibration procedures and results for blunt forebodies

Unknown Author

1999No page data
Forebody flow visualization on the F-18 HARV with actuated forebody strakesDavid F. Fisher

Forebody flow visualization on the F-18 HARV with actuated forebody strakes

David F. Fisher

1998No page data
Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight dataMichael D. Messina

Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data

Michael D. Messina

1995No page data
Experimental and computational aerothermodynamics of a Mars entry vehicleBrian R. Hollis

Experimental and computational aerothermodynamics of a Mars entry vehicle

Brian R. Hollis

1996No page data
Wind code application to external forebody flowfields with comparisons to experimental resultsF. C. Frate

Wind code application to external forebody flowfields with comparisons to experimental results

F. C. Frate

2001No page data
Hi-alpha forebody designWilliam H. Mason

Hi-alpha forebody design

William H. Mason

1992No page data
Optimum shape of a blunt forebody in hypersonic flowL. Maestrello

Optimum shape of a blunt forebody in hypersonic flow

L. Maestrello

1989No page data
Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flowsD. J. Singh

Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows

D. J. Singh

1990No page data
Numerical analysis of tangential slot blowing on a generic chined forebodyRoxana M. Agosta

Numerical analysis of tangential slot blowing on a generic chined forebody

Roxana M. Agosta

1994No page data
Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnelPaul M. Siemers

Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel

Paul M. Siemers

1986No page data
Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60⁰ half-angle chine forebodyHolly M. Ross

Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60⁰ half-angle chine forebody

Holly M. Ross

1997No page data
Inlet flowfield investigationUnknown Author

Inlet flowfield investigation

Unknown Author

1984No page data
F-18 High Alpha Research Vehicle surface pressuresDavid F. Fisher
⏱ 36m

F-18 High Alpha Research Vehicle surface pressures

David F. Fisher

199036 pp.
Effect of curvature on the impact damage characteritiscs and residual strength of composite platesDamodar R. Ambur

Effect of curvature on the impact damage characteritiscs and residual strength of composite plates

Damodar R. Ambur

1998No page data
Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnelPaul M. Siemers

Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel

Paul M. Siemers

1986No page data
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