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		No cover image available Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment by . Series: NASA TM 4032 : 1988Edition: Language: English Publication details: Washington, D.C. ; National Aeronautics and Space Admin ; 1988Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: LNASA TM 4032 : 1988. Add to cart (remove)
		No cover image available Three-step Labyrinth seal for high-performance turbomachines by . Series: NASA TP 1848 : 1987Edition: Language: English Publication details: Washington, D.C. ; National Aeronautics and Space Admin ; 1987Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: LNASA TP 1848 : 1987. Add to cart (remove)
		No cover image available Three-step cylindrical seal for high-performance turbomachines by . Series: NASA TP 1849 : 1987Edition: Language: English Publication details: Washington, D.C. ; National Aeronautics and Space Admin ; 1987Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: NASA TP 1849 : 1987. Add to cart (remove)
		No cover image available Straight cylindrical seal for high-performance turbomachines by . Series: NASA TP 1850 : 1987Edition: Language: English Publication details: Washington, D.C. ; National Aeronautics and Space Admin ; 1987Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: LNASA TP 1850 : 1987. Add to cart (remove)
		No cover image available Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds by . Series: NASA TP 2588 : 1987Edition: Language: English Publication details: Washington, D.C. ; National Aeronautics and Space Admin ; 1987Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: LNASA TP 2588 : 1987. Add to cart (remove)
		No cover image available Second-order accurate kinetic-theory-based method for inviscid compressible flows by . Series: NASA TP 2613 : 1986Edition: Language: English Publication details: Washington, D.C. ; National Aeronautics and Space Admin ; 1986Online access: Click here to access online Availability: Items available for reference: Not for loan (1) Call number: LNASA TP 2613 : 1986. Add to cart (remove)

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