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Cover image for Experimental surface pressure data obtained on 65� delta wing across Reynolds number and Mach number ranges

Experimental surface pressure data obtained on 65� delta wing across Reynolds number and Mach number ranges

by Chu, Julio
1996
Format: Book

Location	Call #	Status
Joyner - Microforms B300	NAS 1.15:4645	✔ Available

Cover image for Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges

Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges

by Chu, Julio
1996
Format: Electronic

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Cover image for High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions

High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions

by Chu, Julio
1990
Format: Book

Location	Call #	Status
Joyner - Microforms B300	NAS 1.15:4227	✔ Available

Cover image for Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°

Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8° to 90°

by Mulcay, William
1980
Format: Electronic

Location
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